def moment(ship, draft=None,
roll=Units.parseQuantity("0 deg"),
trim=Units.parseQuantity("0 deg")):
"""Compute the moment required to trim the ship 1cm
Position arguments:
ship -- Ship object (see createShip)
Keyword arguments:
draft -- Ship draft (Design ship draft by default)
roll -- Roll angle (0 degrees by default)
trim -- Trim angle (0 degrees by default)
Returned value:
Moment required to trim the ship 1cm. Such moment is positive if it cause a
positive trim angle. The moment is expressed as a mass by a distance, not as
a force by a distance
"""
disp_orig, B_orig, _ = displacement(ship, draft, roll, trim)
xcb_orig = Units.Quantity(B_orig.x, Units.Length)
factor = 10.0
x = 0.5 * ship.Length.getValueAs('cm').Value
y = 1.0
angle = math.atan2(y, x) * Units.Radian
trim_new = trim + factor * angle
disp_new, B_new, _ = displacement(ship, draft, roll, trim_new)
xcb_new = Units.Quantity(B_new.x, Units.Length)
mom0 = -disp_orig * xcb_orig
mom1 = -disp_new * xcb_new
return (mom1 - mom0) / factor
def solve(ship, weights, tanks, rolls, var_trim=True):
"""Compute the ship GZ stability curve
Position arguments:
ship -- Ship object
weights -- List of weights to consider
tanks -- List of tanks to consider (each one should be a tuple with the
tank instance, the density of the fluid inside, and the filling level ratio)
rolls -- List of roll angles
Keyword arguments:
var_trim -- True if the equilibrium trim should be computed for each roll
angle, False if null trim angle can be used instead.
Returned value:
List of GZ curve points. Each point contains the GZ stability length, the
equilibrium draft, and the equilibrium trim angle (0 deg if var_trim is
False)
"""
# Get the unloaded weight (ignoring the tanks for the moment).
W = Units.parseQuantity("0 kg")
mom_x = Units.parseQuantity("0 kg*m")
mom_y = Units.parseQuantity("0 kg*m")
mom_z = Units.parseQuantity("0 kg*m")
for w in weights:
W += w.Proxy.getMass(w)
m = w.Proxy.getMoment(w)
mom_x += m[0]
mom_y += m[1]
mom_z += m[2]
COG = Vector(mom_x / W, mom_y / W, mom_z / W)
W = W * G
# Get the tanks weight
TW = Units.parseQuantity("0 kg")
VOLS = []
for t in tanks:
# t[0] = tank object
# t[1] = load density
# t[2] = filling level
vol = t[0].Proxy.getVolume(t[0], t[2])
VOLS.append(vol)
TW += vol * t[1]
TW = TW * G
points = []
for i,roll in enumerate(rolls):
App.Console.PrintMessage("{0} / {1}\n".format(i + 1, len(rolls)))
point = solve_point(W, COG, TW, VOLS,
ship, tanks, roll, var_trim)
if point is None:
return []
points.append(point)
return points
def floatingArea(ship, draft=None,
roll=Units.parseQuantity("0 deg"),
trim=Units.parseQuantity("0 deg")):
"""Compute the ship floating area
Position arguments:
ship -- Ship object (see createShip)
Keyword arguments:
draft -- Ship draft (Design ship draft by default)
roll -- Roll angle (0 degrees by default)
trim -- Trim angle (0 degrees by default)
Returned values:
area -- Ship floating area
cf -- Floating area coefficient
"""
if draft is None:
draft = ship.Draft
# We want to intersect the whole ship with the free surface, so in this case
# we must not use the underwater side (or the tool will fail)
shape, _ = placeShipShape(ship.Shape.copy(), draft, roll, trim)
try:
f = Part.Face(shape.slice(Vector(0,0,1), 0.0))
area = Units.Quantity(f.Area, Units.Area)
except Part.OCCError:
msg = QtGui.QApplication.translate(
"ship_console",
"Part.OCCError: Floating area cannot be computed",
None)
App.Console.PrintError(msg + '\n')
area = Units.Quantity(0.0, Units.Area)
bbox = shape.BoundBox
Area = (bbox.XMax - bbox.XMin) * (bbox.YMax - bbox.YMin)
try:
cf = area.Value / Area
except ZeroDivisionError:
msg = QtGui.QApplication.translate(
"ship_console",
"ZeroDivisionError: Null area found during the floating area"
" computation!",
None)
App.Console.PrintError(msg + '\n')
cf = 0.0
return area, cf
def mainFrameCoeff(ship, draft=None):
"""Compute the main frame coefficient
Position arguments:
ship -- Ship object (see createShip)
Keyword arguments:
draft -- Ship draft (Design ship draft by default)
Returned value:
Ship main frame area coefficient
"""
if draft is None:
draft = ship.Draft
shape, _ = placeShipShape(ship.Shape.copy(), draft,
Units.parseQuantity("0 deg"),
Units.parseQuantity("0 deg"))
shape = getUnderwaterSide(shape)
try:
f = Part.Face(shape.slice(Vector(1,0,0), 0.0))
area = f.Area
except Part.OCCError:
msg = QtGui.QApplication.translate(
"ship_console",
"Part.OCCError: Main frame area cannot be computed",
None)
App.Console.PrintError(msg + '\n')
area = 0.0
bbox = shape.BoundBox
Area = (bbox.YMax - bbox.YMin) * (bbox.ZMax - bbox.ZMin)
try:
cm = area / Area
except ZeroDivisionError:
msg = QtGui.QApplication.translate(
"ship_console",
"ZeroDivisionError: Null area found during the main frame area"
" coefficient computation!",
None)
App.Console.PrintError(msg + '\n')
cm = 0.0
return cm
def accept(self):
"""Create the ship instance"""
mw = self.getMainWindow()
form = mw.findChild(QtGui.QWidget, "TaskPanel")
form.ship = self.widget(QtGui.QComboBox, "Ship")
form.weight = self.widget(QtGui.QLineEdit, "Weight")
ship = self.ships[form.ship.currentIndex()]
density = Units.parseQuantity(Locale.fromString(form.weight.text()))
Tools.createWeight(self.shapes, ship, density)
return True
def wettedArea(shape, draft, roll=Units.parseQuantity("0 deg"),
trim=Units.parseQuantity("0 deg")):
"""Compute the ship wetted area
Position arguments:
shape -- External faces of the ship hull
draft -- Ship draft
Keyword arguments:
roll -- Roll angle (0 degrees by default)
trim -- Trim angle (0 degrees by default)
Returned value:
The wetted area, i.e. The underwater side area
"""
shape, _ = placeShipShape(shape.copy(), draft, roll, trim)
shape = getUnderwaterSide(shape, force=False)
area = 0.0
for f in shape.Faces:
area = area + f.Area
return Units.Quantity(area, Units.Area)
def BMT(ship, draft=None, trim=Units.parseQuantity("0 deg")):
"""Calculate "ship Bouyance center" - "transversal metacenter" radius
Position arguments:
ship -- Ship object (see createShip)
Keyword arguments:
draft -- Ship draft (Design ship draft by default)
trim -- Trim angle (0 degrees by default)
Returned value:
BMT radius
"""
if draft is None:
draft = ship.Draft
roll = Units.parseQuantity("0 deg")
_, B0, _ = displacement(ship, draft, roll, trim)
nRoll = 2
maxRoll = Units.parseQuantity("7 deg")
BM = 0.0
for i in range(nRoll):
roll = (maxRoll / nRoll) * (i + 1)
_, B1, _ = displacement(ship, draft, roll, trim)
# * M
# / \
# / \ BM ==|> BM = (BB/2) / sin(alpha/2)
# / \
# *-------*
# BB
BB = B1 - B0
BB.x = 0.0
# nRoll is actually representing the weight function
BM += 0.5 * BB.Length / math.sin(math.radians(0.5 * roll)) / nRoll
return Units.Quantity(BM, Units.Length)
def solve_point(W, COG, TW, VOLS, ship, tanks, roll, var_trim=True):
""" Compute the ship GZ value.
@param W Empty ship weight.
@param COG Empty ship Center of mass.
@param TW Tanks weights.
@param VOLS List of tank volumes.
@param tanks Considered tanks.
@param roll Roll angle.
@param var_trim True if the trim angle should be recomputed at each roll
angle, False otherwise.
@return GZ value, equilibrium draft, and equilibrium trim angle (0 if
variable trim has not been requested)
"""
# Look for the equilibrium draft (and eventually the trim angle too)
max_draft = Units.Quantity(ship.Shape.BoundBox.ZMax, Units.Length)
draft = ship.Draft
max_disp = Units.Quantity(ship.Shape.Volume, Units.Volume) * DENS * G
if max_disp < W + TW:
msg = QtGui.QApplication.translate(
"ship_console",
"Too much weight! The ship will never displace water enough",
None)
App.Console.PrintError(msg + ' ({} vs. {})\n'.format(
(max_disp / G).UserString, ((W + TW) / G).UserString))
return None
trim = Units.parseQuantity("0 deg")
for i in range(MAX_EQUILIBRIUM_ITERS):
# Get the displacement, and the bouyance application point
disp, B, _ = Hydrostatics.displacement(ship,
draft,
roll,
trim)
disp *= G
# Add the tanks effect on the center of gravity
mom_x = Units.Quantity(COG.x, Units.Length) * W
mom_y = Units.Quantity(COG.y, Units.Length) * W
mom_z = Units.Quantity(COG.z, Units.Length) * W
for i,t in enumerate(tanks):
tank_weight = VOLS[i] * t[1] * G
tank_cog = t[0].Proxy.getCoG(t[0], VOLS[i], roll, trim)
mom_x += Units.Quantity(tank_cog.x, Units.Length) * tank_weight
mom_y += Units.Quantity(tank_cog.y, Units.Length) * tank_weight
mom_z += Units.Quantity(tank_cog.z, Units.Length) * tank_weight
cog_x = mom_x / (W + TW)
cog_y = mom_y / (W + TW)
cog_z = mom_z / (W + TW)
# Compute the errors
draft_error = -((disp - W - TW) / max_disp).Value
R_x = cog_x - Units.Quantity(B.x, Units.Length)
R_y = cog_y - Units.Quantity(B.y, Units.Length)
R_z = cog_z - Units.Quantity(B.z, Units.Length)
if not var_trim:
trim_error = 0.0
else:
trim_error = -TRIM_RELAX_FACTOR * R_x / ship.Length
# Check if we can tolerate the errors
if abs(draft_error) < 0.01 and abs(trim_error) < 0.1:
break
# Get the new draft and trim
draft += draft_error * max_draft
trim += trim_error * Units.Degree
# GZ should be provided in the Free surface oriented frame of reference
c = math.cos(roll.getValueAs('rad'))
s = math.sin(roll.getValueAs('rad'))
return c * R_y - s * R_z, draft, trim
def areas(ship, n, draft=None,
roll=Units.parseQuantity("0 deg"),
trim=Units.parseQuantity("0 deg")):
"""Compute the ship transversal areas
Position arguments:
ship -- Ship object (see createShip)
n -- Number of points to compute
Keyword arguments:
draft -- Ship draft (Design ship draft by default)
roll -- Roll angle (0 degrees by default)
trim -- Trim angle (0 degrees by default)
Returned value:
List of sections, each section contains 2 values, the x longitudinal
coordinate, and the transversal area. If n < 2, an empty list will be
returned.
"""
if n < 2:
return []
if draft is None:
draft = ship.Draft
shape, _ = placeShipShape(ship.Shape.copy(), draft, roll, trim)
shape = getUnderwaterSide(shape)
# Sections distance computation
bbox = shape.BoundBox
xmin = bbox.XMin
xmax = bbox.XMax
dx = (xmax - xmin) / (n - 1.0)
# Since we are computing the sections in the total length (not in the
# length between perpendiculars), we can grant that the starting and
# ending sections have null area
areas = [(Units.Quantity(xmin, Units.Length),
Units.Quantity(0.0, Units.Area))]
# And since we just need to compute areas we will create boxes with its
# front face at the desired transversal area position, computing the
# common solid part, dividing it by faces, and getting only the desired
# ones.
App.Console.PrintMessage("Computing transversal areas...\n")
App.Console.PrintMessage("Some Inventor representation errors can be"
" shown, please ignore them.\n")
for i in range(1, n - 1):
App.Console.PrintMessage("{0} / {1}\n".format(i, n - 2))
x = xmin + i * dx
try:
f = Part.Face(shape.slice(Vector(1,0,0), x))
except Part.OCCError:
msg = QtGui.QApplication.translate(
"ship_console",
"Part.OCCError: Transversal area computation failed",
None)
App.Console.PrintError(msg + '\n')
areas.append((Units.Quantity(x, Units.Length),
Units.Quantity(0.0, Units.Area)))
continue
# It is a valid face, so we can add this area
areas.append((Units.Quantity(x, Units.Length),
Units.Quantity(f.Area, Units.Area)))
# Last area is equal to zero (due to the total length usage)
areas.append((Units.Quantity(xmax, Units.Length),
Units.Quantity(0.0, Units.Area)))
App.Console.PrintMessage("Done!\n")
return areas
def get_boundary_layer_data(self):
# mesh boundary layer
# currently only one boundary layer setting object is allowed
# but multiple boundary can be selected
# Mesh.CharacteristicLengthMin, must be zero
# or a value less than first inflation layer height
if not self.mesh_obj.MeshBoundaryLayerList:
# print(" No mesh boundary layer setting document object.")
pass
else:
Console.PrintMessage(
" Mesh boundary layers, we need to get the elements.\n")
if self.part_obj.Shape.ShapeType == "Compound":
# see http://forum.freecadweb.org/viewtopic.php?f=18&t=18780&start=40#p149467 and
# http://forum.freecadweb.org/viewtopic.php?f=18&t=18780&p=149520#p149520
err = (
"Gmsh could return unexpected meshes for a boolean split tools Compound. "
"It is strongly recommended to extract the shape to mesh "
"from the Compound and use this one.")
Console.PrintError(err + "\n")
for mr_obj in self.mesh_obj.MeshBoundaryLayerList:
if mr_obj.MinimumThickness and Units.Quantity(
mr_obj.MinimumThickness).Value > 0:
if mr_obj.References:
belem_list = []
for sub in mr_obj.References:
# print(sub[0]) # Part the elements belongs to
# check if the shape of the mesh boundary_layer is an
# element of the Part to mesh
# if not try to find the element in the shape to mesh
search_ele_in_shape_to_mesh = False
if not self.part_obj.Shape.isSame(sub[0].Shape):
Console.PrintLog(
" One element of the mesh boundary layer {} is "
"not an element of the Part to mesh.\n"
"But we are going to try to find it in "
"the Shape to mesh :-)\n".format(
mr_obj.Name))
search_ele_in_shape_to_mesh = True
for elems in sub[1]:
# print(elems) # elems --> element
if search_ele_in_shape_to_mesh:
# we try to find the element it in the Shape to mesh
# and use the found element as elems
# the method getElement(element) does not return Solid elements
ele_shape = meshtools.get_element(
sub[0], elems)
found_element = meshtools.find_element_in_shape(
self.part_obj.Shape, ele_shape)
if found_element: # also
elems = found_element
else:
Console.PrintError(
"One element of the mesh boundary layer {} could "
"not be found in the Part to mesh. "
"It will be ignored.\n".format(
mr_obj.Name))
# print(elems) # element
if elems not in self.bl_boundary_list:
# fetch settings in DocumentObject
# fan setting is not implemented
belem_list.append(elems)
self.bl_boundary_list.append(elems)
else:
Console.PrintError(
"The element {} of the mesh boundary "
"layer {} has been added "
"to another mesh boundary layer.\n".
format(elems, mr_obj.Name))
setting = {}
setting["hwall_n"] = Units.Quantity(
mr_obj.MinimumThickness).Value
setting["ratio"] = mr_obj.GrowthRate
setting["thickness"] = sum([
setting["hwall_n"] * setting["ratio"]**i
for i in range(mr_obj.NumberOfLayers)
])
# setting["hwall_n"] * 5 # tangential cell dimension
setting["hwall_t"] = setting["thickness"]
# hfar: cell dimension outside boundary
# should be set later if some character length is set
if self.clmax > setting["thickness"] * 0.8 \
and self.clmax < setting["thickness"] * 1.6:
setting["hfar"] = self.clmax
else:
# set a value for safety, it may works as background mesh cell size
setting["hfar"] = setting["thickness"]
# from face name -> face id is done in geo file write up
# TODO: fan angle setup is not implemented yet
if self.dimension == "2":
setting["EdgesList"] = belem_list
elif self.dimension == "3":
setting["FacesList"] = belem_list
else:
Console.PrintError(
"boundary layer is only supported for 2D and 3D mesh"
)
self.bl_setting_list.append(setting)
else:
Console.PrintError(
"The mesh boundary layer: {} is not used to create "
"the mesh because the reference list is empty.\n".
format(mr_obj.Name))
else:
Console.PrintError(
"The mesh boundary layer: {} is not used to create "
"the mesh because the min thickness is 0.0 mm.\n".
format(mr_obj.Name))
Console.PrintMessage(" {}\n".format(self.bl_setting_list))
def gz(lc, rolls, var_trim=True):
"""Compute the ship GZ stability curve
Position arguments:
lc -- Load condition spreadsheet
rolls -- List of roll angles to compute
Keyword arguments:
var_trim -- True if the equilibrium trim should be computed for each roll
angle, False if null trim angle can be used instead.
Returned value:
List of GZ curve points. Each point contains the GZ stability length, the
equilibrium draft, and the equilibrium trim angle (0 deg if var_trim is
False)
"""
# B1 cell must be a ship
# B2 cell must be the loading condition itself
doc = lc.Document
try:
if lc not in doc.getObjectsByLabel(lc.get('B2')):
return[]
ships = doc.getObjectsByLabel(lc.get('B1'))
if len(ships) != 1:
if len(ships) == 0:
msg = QtGui.QApplication.translate(
"ship_console",
"Wrong Ship label! (no instances labeled as"
"'{}' found)",
None)
App.Console.PrintError(msg + '\n'.format(
lc.get('B1')))
else:
msg = QtGui.QApplication.translate(
"ship_console",
"Ambiguous Ship label! ({} instances labeled as"
"'{}' found)",
None)
App.Console.PrintError(msg + '\n'.format(
len(ships),
lc.get('B1')))
return[]
ship = ships[0]
if ship is None or not ship.PropertiesList.index("IsShip"):
return[]
except ValueError:
return[]
# Extract the weights and the tanks
weights = []
index = 6
while True:
try:
ws = doc.getObjectsByLabel(lc.get('A{}'.format(index)))
except ValueError:
break
index += 1
if len(ws) != 1:
if len(ws) == 0:
msg = QtGui.QApplication.translate(
"ship_console",
"Wrong Weight label! (no instances labeled as"
"'{}' found)",
None)
App.Console.PrintError(msg + '\n'.format(
lc.get('A{}'.format(index - 1))))
else:
msg = QtGui.QApplication.translate(
"ship_console",
"Ambiguous Weight label! ({} instances labeled as"
"'{}' found)",
None)
App.Console.PrintError(msg + '\n'.format(
len(ws),
lc.get('A{}'.format(index - 1))))
continue
w = ws[0]
try:
if w is None or not w.PropertiesList.index("IsWeight"):
msg = QtGui.QApplication.translate(
"ship_console",
"Invalid Weight! (the object labeled as"
"'{}' is not a weight)",
None)
App.Console.PrintError(msg + '\n'.format(
len(ws),
lc.get('A{}'.format(index - 1))))
continue
except ValueError:
continue
weights.append(w)
tanks = []
index = 6
while True:
try:
ts = doc.getObjectsByLabel(lc.get('C{}'.format(index)))
dens = float(lc.get('D{}'.format(index)))
level = float(lc.get('E{}'.format(index)))
dens = Units.parseQuantity("{} kg/m^3".format(dens))
except ValueError:
break
index += 1
if len(ts) != 1:
if len(ts) == 0:
msg = QtGui.QApplication.translate(
"ship_console",
"Wrong Tank label! (no instances labeled as"
"'{}' found)",
None)
App.Console.PrintError(msg + '\n'.format(
lc.get('C{}'.format(index - 1))))
else:
msg = QtGui.QApplication.translate(
"ship_console",
"Ambiguous Tank label! ({} instances labeled as"
"'{}' found)",
None)
App.Console.PrintError(msg + '\n'.format(
len(ts),
lc.get('C{}'.format(index - 1))))
continue
t = ts[0]
try:
if t is None or not t.PropertiesList.index("IsTank"):
msg = QtGui.QApplication.translate(
"ship_console",
"Invalid Tank! (the object labeled as"
"'{}' is not a tank)",
None)
App.Console.PrintError(msg + '\n'.format(
len(ws),
lc.get('C{}'.format(index - 1))))
continue
except ValueError:
continue
tanks.append((t, dens, level))
return solve(ship, weights, tanks, rolls, var_trim)
def getFromUi(value, unit, outputDim):
quantity = Units.Quantity(str(value) + str(unit))
return convert(quantity, outputDim)
def get_region_data(self):
# mesh regions
if not self.mesh_obj.MeshRegionList:
# print(" No mesh regions.")
pass
else:
Console.PrintMessage(
' Mesh regions, we need to get the elements.\n')
# by the use of MeshRegion object and a BooleanSplitCompound
# there could be problems with node numbers see
# http://forum.freecadweb.org/viewtopic.php?f=18&t=18780&start=40#p149467
# http://forum.freecadweb.org/viewtopic.php?f=18&t=18780&p=149520#p149520
part = self.part_obj
if self.mesh_obj.MeshRegionList:
# other part obj might not have a Proxy, thus an exception would be raised
if part.Shape.ShapeType == "Compound" and hasattr(
part, "Proxy"):
if part.Proxy.Type == "FeatureBooleanFragments" \
or part.Proxy.Type == "FeatureSlice" \
or part.Proxy.Type == "FeatureXOR":
error_message = (
" The mesh to shape is a boolean split tools Compound "
"and the mesh has mesh region list. "
"Gmsh could return unexpected meshes in such circumstances. "
"It is strongly recommended to extract the shape to mesh "
"from the Compound and use this one.")
Console.PrintError(error_message + "\n")
# TODO: no gui popup because FreeCAD will be in a endless output loop
# as long as the pop up is on --> maybe find a better solution for
# either of both --> thus the pop up is in task panel
for mr_obj in self.mesh_obj.MeshRegionList:
# print(mr_obj.Name)
# print(mr_obj.CharacteristicLength)
# print(Units.Quantity(mr_obj.CharacteristicLength).Value)
if mr_obj.CharacteristicLength:
if mr_obj.References:
for sub in mr_obj.References:
# print(sub[0]) # Part the elements belongs to
# check if the shape of the mesh region
# is an element of the Part to mesh
# if not try to find the element in the shape to mesh
search_ele_in_shape_to_mesh = False
if not self.part_obj.Shape.isSame(sub[0].Shape):
Console.PrintLog(
" One element of the meshregion {} is "
"not an element of the Part to mesh.\n"
"But we are going to try to find it in "
"the Shape to mesh :-)\n".format(
mr_obj.Name))
search_ele_in_shape_to_mesh = True
for elems in sub[1]:
# print(elems) # elems --> element
if search_ele_in_shape_to_mesh:
# we're going to try to find the element in the
# Shape to mesh and use the found element as elems
# the method getElement(element)
# does not return Solid elements
ele_shape = meshtools.get_element(
sub[0], elems)
found_element = meshtools.find_element_in_shape(
self.part_obj.Shape, ele_shape)
if found_element:
elems = found_element
else:
Console.PrintError(
"One element of the meshregion {} could not be found "
"in the Part to mesh. It will be ignored.\n"
.format(mr_obj.Name))
# print(elems) # element
if elems not in self.ele_length_map:
self.ele_length_map[
elems] = Units.Quantity(
mr_obj.CharacteristicLength).Value
else:
Console.PrintError(
"The element {} of the meshregion {} has "
"been added to another mesh region.\n".
format(elems, mr_obj.Name))
else:
Console.PrintError(
"The meshregion: {} is not used to create the mesh "
"because the reference list is empty.\n".format(
mr_obj.Name))
else:
Console.PrintError(
"The meshregion: {} is not used to create the "
"mesh because the CharacteristicLength is 0.0 mm.\n".
format(mr_obj.Name))
for eleml in self.ele_length_map:
# the method getElement(element) does not return Solid elements
ele_shape = meshtools.get_element(self.part_obj, eleml)
ele_vertexes = meshtools.get_vertexes_by_element(
self.part_obj.Shape, ele_shape)
self.ele_node_map[eleml] = ele_vertexes
Console.PrintMessage(" {}\n".format(self.ele_length_map))
Console.PrintMessage(" {}\n".format(self.ele_node_map))
def check_material_keys(self):
# FreeCAD units definition is at file end of src/Base/Unit.cpp
if not self.material:
FreeCAD.Console.PrintMessage(
"For some reason all material data is empty!\n")
self.material["Name"] = "NoName"
if "Density" in self.material:
if "Density" not in str(Units.Unit(self.material["Density"])):
FreeCAD.Console.PrintMessage(
"Density in material data seems to have no unit "
"or a wrong unit (reset the value): {}\n".format(
self.material["Name"]))
self.material["Density"] = "0 kg/m^3"
else:
FreeCAD.Console.PrintMessage("Density not found in {}\n".format(
self.material["Name"]))
self.material["Density"] = "0 kg/m^3"
if self.obj.Category == "Solid":
# mechanical properties
if "YoungsModulus" in self.material:
# unit type of YoungsModulus is Pressure
if "Pressure" not in str(
Units.Unit(self.material["YoungsModulus"])):
FreeCAD.Console.PrintMessage(
"YoungsModulus in material data seems to have no unit "
"or a wrong unit (reset the value): {}\n".format(
self.material["Name"]))
self.material["YoungsModulus"] = "0 MPa"
else:
FreeCAD.Console.PrintMessage(
"YoungsModulus not found in {}\n".format(
self.material["Name"]))
self.material["YoungsModulus"] = "0 MPa"
if "PoissonRatio" in self.material:
# PoissonRatio does not have a unit, but it is checked it there is no value at all
try:
float(self.material["PoissonRatio"])
except ValueError:
FreeCAD.Console.PrintMessage(
"PoissonRatio has wrong or no data (reset the value): {}\n"
.format(self.material["PoissonRatio"]))
self.material["PoissonRatio"] = "0"
else:
FreeCAD.Console.PrintMessage(
"PoissonRatio not found in {}\n".format(
self.material["Name"]))
self.material["PoissonRatio"] = "0"
if self.obj.Category == "Fluid":
# Fluidic properties
if "KinematicViscosity" in self.material:
ki_vis = self.material["KinematicViscosity"]
if "KinematicViscosity" not in str(Units.Unit(ki_vis)):
FreeCAD.Console.PrintMessage(
"KinematicViscosity in material data seems to have no unit "
"or a wrong unit (reset the value): {}\n".format(
self.material["Name"]))
self.material["KinematicViscosity"] = "0 m^2/s"
else:
FreeCAD.Console.PrintMessage(
"KinematicViscosity not found in {}\n".format(
self.material["Name"]))
self.material["KinematicViscosity"] = "0 m^2/s"
if "VolumetricThermalExpansionCoefficient" in self.material:
# unit type VolumetricThermalExpansionCoefficient is ThermalExpansionCoefficient
vol_ther_ex_co = self.material[
"VolumetricThermalExpansionCoefficient"]
if "VolumetricThermalExpansionCoefficient" not in str(
Units.Unit(vol_ther_ex_co)):
FreeCAD.Console.PrintMessage(
"VolumetricThermalExpansionCoefficient in material data "
"seems to have no unit or a wrong unit (reset the value): {}\n"
.format(self.material["Name"]))
self.material[
"VolumetricThermalExpansionCoefficient"] = "0 m^3/m^3/K"
else:
FreeCAD.Console.PrintMessage(
"VolumetricThermalExpansionCoefficient not found in {}\n".
format(self.material["Name"]))
self.material[
"VolumetricThermalExpansionCoefficient"] = "0 m^3/m^3/K"
# Thermal properties
if "ThermalConductivity" in self.material:
if "ThermalConductivity" not in str(
Units.Unit(self.material["ThermalConductivity"])):
FreeCAD.Console.PrintMessage(
"ThermalConductivity in material data seems to have no unit "
"or a wrong unit (reset the value): {}\n".format(
self.material["Name"]))
self.material["ThermalConductivity"] = "0 W/m/K"
else:
FreeCAD.Console.PrintMessage(
"ThermalConductivity not found in {}\n".format(
self.material["Name"]))
self.material["ThermalConductivity"] = "0 W/m/K"
if "ThermalExpansionCoefficient" in self.material:
the_ex_co = self.material["ThermalExpansionCoefficient"]
if "ThermalExpansionCoefficient" not in str(Units.Unit(the_ex_co)):
FreeCAD.Console.PrintMessage(
"ThermalExpansionCoefficient in material data seems to have no unit "
"or a wrong unit (reset the value): {}\n".format(
self.material["Name"]))
self.material["ThermalExpansionCoefficient"] = "0 um/m/K"
else:
FreeCAD.Console.PrintMessage(
"ThermalExpansionCoefficient not found in {}\n".format(
self.material["Name"]))
self.material["ThermalExpansionCoefficient"] = "0 um/m/K"
if "SpecificHeat" in self.material:
if "SpecificHeat" not in str(
Units.Unit(self.material["SpecificHeat"])):
FreeCAD.Console.PrintMessage(
"SpecificHeat in material data seems to have no unit "
"or a wrong unit (reset the value): {}\n".format(
self.material["Name"]))
self.material["SpecificHeat"] = "0 J/kg/K"
else:
FreeCAD.Console.PrintMessage(
"SpecificHeat not found in {}\n".format(self.material["Name"]))
self.material["SpecificHeat"] = "0 J/kg/K"
FreeCAD.Console.PrintMessage("\n")
def processRefinements(self):
""" Process mesh refinements """
mr_objs = CfdTools.getMeshRefinementObjs(self.mesh_obj)
cf_settings = self.cf_settings
cf_settings['MeshRegions'] = {}
cf_settings['BoundaryLayers'] = {}
cf_settings['InternalRegions'] = {}
snappy_settings = self.snappy_settings
snappy_settings['MeshRegions'] = {}
snappy_settings['BoundaryLayers'] = {}
snappy_settings['InternalRegions'] = {}
# Make list of all faces in meshed shape with original index
mesh_face_list = list(
zip(self.mesh_obj.Part.Shape.Faces,
range(len(self.mesh_obj.Part.Shape.Faces))))
# Make list of all boundary references
CfdTools.cfdMessage("Matching boundary patches\n")
boundary_face_list = []
bc_group = None
analysis_obj = CfdTools.getParentAnalysisObject(self.mesh_obj)
if not analysis_obj:
analysis_obj = CfdTools.getActiveAnalysis()
if analysis_obj:
bc_group = CfdTools.getCfdBoundaryGroup(analysis_obj)
for bc_id, bc_obj in enumerate(bc_group):
for ri, ref in enumerate(bc_obj.ShapeRefs):
try:
bf = CfdTools.resolveReference(ref)
except RuntimeError as re:
raise RuntimeError(
"Error processing boundary condition {}: {}".format(
bc_obj.Label, str(re)))
for si, s in enumerate(bf):
boundary_face_list += [(sf, (bc_id, ri, si))
for sf in s[0].Faces]
# Match them up to faces in the main geometry
bc_matched_faces = CfdTools.matchFaces(boundary_face_list,
mesh_face_list)
# Check for and filter duplicates
bc_match_per_shape_face = [-1] * len(mesh_face_list)
for k in range(len(bc_matched_faces)):
match = bc_matched_faces[k][1]
prev_k = bc_match_per_shape_face[match]
if prev_k >= 0:
nb, ri, si = bc_matched_faces[k][0]
nb2, ri2, si2 = bc_matched_faces[prev_k][0]
bc = bc_group[nb]
bc2 = bc_group[nb2]
CfdTools.cfdWarning(
"Boundary '{}' reference {}:{} also assigned as "
"boundary '{}' reference {}:{} - ignoring duplicate\n".
format(bc.Label, bc.ShapeRefs[ri][0].Name,
bc.ShapeRefs[ri][1][si], bc2.Label,
bc.ShapeRefs[ri][0].Name, bc.ShapeRefs[ri][1][si]))
else:
bc_match_per_shape_face[match] = k
# Match relevant mesh regions to the shape being meshed: boundary layer mesh regions for cfMesh,
# all surface mesh refinements for snappyHexMesh, and extrusion patches for all meshers.
# For cfMesh, surface mesh refinements are written as separate surfaces so need not be matched
CfdTools.cfdMessage("Matching mesh refinement regions\n")
mr_face_list = []
for mr_id, mr_obj in enumerate(mr_objs):
if mr_obj.Extrusion or (
self.mesh_obj.MeshUtility == 'cfMesh'
and not mr_obj.Internal and mr_obj.NumberLayers > 0) or (
self.mesh_obj.MeshUtility == 'snappyHexMesh'
and not mr_obj.Internal):
for ri, r in enumerate(mr_obj.ShapeRefs):
try:
bf = CfdTools.resolveReference(r)
except RuntimeError as re:
raise RuntimeError(
"Error processing mesh refinement {}: {}".format(
mr_obj.Label, str(re)))
for si, s in enumerate(bf):
mr_face_list += [(f, (mr_id, ri, si))
for f in s[0].Faces]
# Match them up to the primary geometry
mr_matched_faces = CfdTools.matchFaces(mr_face_list, mesh_face_list)
# Check for and filter duplicates
mr_match_per_shape_face = [-1] * len(mesh_face_list)
for k in range(len(mr_matched_faces)):
match = mr_matched_faces[k][1]
prev_k = mr_match_per_shape_face[match]
if prev_k >= 0:
nr, ri, si = mr_matched_faces[k][0]
nr2, ri2, si2 = mr_matched_faces[prev_k][0]
CfdTools.cfdWarning(
"Mesh refinement '{}' reference {}:{} also assigned as "
"mesh refinement '{}' reference {}:{} - ignoring duplicate\n"
.format(mr_objs[nr].Label,
mr_objs[nr].ShapeRefs[ri][0].Name,
mr_objs[nr].ShapeRefs[ri][1][si],
mr_objs[nr2].Label,
mr_objs[nr2].ShapeRefs[ri2][0].Name,
mr_objs[nr2].ShapeRefs[ri2][1][si2]))
else:
mr_match_per_shape_face[match] = k
self.patch_faces = []
self.patch_names = []
for k in range(len(bc_group) + 1):
self.patch_faces.append([])
self.patch_names.append([])
for l in range(len(mr_objs) + 1):
self.patch_faces[k].append([])
self.patch_names[k].append("patch_" + str(k) + "_" + str(l))
for i in range(len(mesh_face_list)):
k = bc_match_per_shape_face[i]
l = mr_match_per_shape_face[i]
nb = -1
nr = -1
if k >= 0:
nb, bri, bsi = bc_matched_faces[k][0]
if l >= 0:
nr, rri, ssi = mr_matched_faces[l][0]
self.patch_faces[nb + 1][nr + 1].append(i)
# For gmsh, match mesh refinement with vertices in original mesh
mr_matched_vertices = []
if self.mesh_obj.MeshUtility == 'gmsh':
# Make list of all vertices in meshed shape with original index
mesh_vertices_list = list(
zip(self.mesh_obj.Part.Shape.Vertexes,
range(len(self.mesh_obj.Part.Shape.Vertexes))))
CfdTools.cfdMessage("Matching mesh refinements\n")
mr_vertices_list = []
for mr_id, mr_obj in enumerate(mr_objs):
if not mr_obj.Internal:
for ri, r in enumerate(mr_obj.ShapeRefs):
try:
bf = CfdTools.resolveReference(r)
except RuntimeError as re:
raise RuntimeError(
"Error processing mesh refinement {}: {}".
format(mr_obj.Label, str(re)))
for si, s in enumerate(bf):
mr_vertices_list += [(v, (mr_id, ri, si))
for v in s[0].Vertexes]
mr_matched_vertices = CfdTools.matchFaces(mr_vertices_list,
mesh_vertices_list)
self.ele_length_map = {}
self.ele_node_map = {}
# For snappyHexMesh, also match surface mesh refinements to the boundary conditions, to identify boundary
# conditions on supplementary geometry defined by the surface mesh refinements
# Also matches baffles to surface mesh refinements
bc_mr_matched_faces = []
if self.mesh_obj.MeshUtility == 'snappyHexMesh':
bc_mr_matched_faces = CfdTools.matchFaces(boundary_face_list,
mr_face_list)
# Handle baffles
for bc_id, bc_obj in enumerate(bc_group):
if bc_obj.BoundaryType == 'baffle':
baffle_matches = [
m for m in bc_mr_matched_faces if m[0][0] == bc_id
]
mr_match_per_baffle_ref = []
for r in bc_obj.ShapeRefs:
mr_match_per_baffle_ref += [[-1] * len(r[1])]
for m in baffle_matches:
mr_match_per_baffle_ref[m[0][1]][m[0][2]] = m[1][0]
# For each mesh region, the refs that are part of this baffle
baffle_patch_refs = [[] for ri in range(len(mr_objs) + 1)]
for ri, mr in enumerate(mr_match_per_baffle_ref):
for si, mri in enumerate(mr_match_per_baffle_ref[ri]):
baffle_patch_refs[mri + 1].append(
(bc_obj.ShapeRefs[ri][0],
(bc_obj.ShapeRefs[ri][1][si], )))
# Write these geometries
for ri, refs in enumerate(baffle_patch_refs):
try:
shape = CfdTools.makeShapeFromReferences(refs)
except RuntimeError as re:
raise RuntimeError(
"Error processing baffle {}: {}".format(
bc_obj.Label, str(re)))
solid_name = bc_obj.Name + "_" + str(ri)
if shape:
CfdTools.cfdMessage(
"Triangulating baffle {}, section {}\n".format(
bc_obj.Label, ri))
writeSurfaceMeshFromShape(shape, self.triSurfaceDir,
solid_name, self.mesh_obj)
if ri > 0: # The parts of the baffle corresponding to a surface mesh region obj
mr_obj = mr_objs[ri - 1]
refinement_level = CfdTools.relLenToRefinementLevel(
mr_obj.RelativeLength)
edge_level = CfdTools.relLenToRefinementLevel(
mr_obj.RegionEdgeRefinement)
else: # The parts of the baffle with no refinement obj
refinement_level = 0
edge_level = 0
snappy_settings['MeshRegions'][solid_name] = {
'RefinementLevel': refinement_level,
'EdgeRefinementLevel': edge_level,
'MaxRefinementLevel': max(refinement_level,
edge_level),
'Baffle': True
}
for mr_id, mr_obj in enumerate(mr_objs):
Internal = mr_obj.Internal
mr_rellen = mr_obj.RelativeLength
if mr_rellen > 1.0:
mr_rellen = 1.0
FreeCAD.Console.PrintError(
"The mesh refinement region '{}' should not use a relative length greater "
"than unity.\n".format(mr_obj.Name))
elif mr_rellen < 0.001:
mr_rellen = 0.001 # Relative length should not be less than 0.1% of base length
FreeCAD.Console.PrintError(
"The mesh refinement region '{}' should not use a relative length smaller "
"than 0.001.\n".format(mr_obj.Name))
if self.mesh_obj.MeshUtility == 'gmsh':
# Generate element maps for gmsh
if not Internal:
mesh_vertex_idx = [
mf[1] for mf in mr_matched_vertices
if mf[0][0] == mr_id
]
self.ele_length_map[mr_obj.Name] = mr_rellen * self.clmax
self.ele_node_map[mr_obj.Name] = mesh_vertex_idx
else:
# Find any matches with boundary conditions; mark those matching baffles for removal
bc_matches = [
m for m in bc_mr_matched_faces if m[1][0] == mr_id
]
bc_match_per_mr_ref = []
for ri, r in enumerate(mr_obj.ShapeRefs):
bc_match_per_mr_ref.append([-1] * len(r[1]))
for m in bc_matches:
bc_match_per_mr_ref[m[1][1]][m[1][2]] = -2 if bc_group[
m[0][0]].BoundaryType == 'baffle' else m[0][0]
# Unmatch those in primary geometry
main_geom_matches = [
m for m in mr_matched_faces if m[0][0] == mr_id
]
for m in main_geom_matches:
bc_match_per_mr_ref[m[0][1]][m[0][2]] = -1
# For each boundary, the refs that are part of this mesh region
mr_patch_refs = [[] for ri in range(len(bc_group) + 1)]
for ri, m in enumerate(bc_match_per_mr_ref):
for si, bci in enumerate(m):
if bci > -2:
mr_patch_refs[bci + 1].append(
(mr_obj.ShapeRefs[ri][0],
(mr_obj.ShapeRefs[ri][1][si], )))
# Loop over and write the sub-sections of this mesh object
for bi in range(len(mr_patch_refs)):
if len(mr_patch_refs[bi]) and not mr_obj.Extrusion:
if bi == 0:
mr_patch_name = mr_obj.Name
else:
mr_patch_name = self.patch_names[bi][mr_id + 1]
CfdTools.cfdMessage(
"Triangulating mesh refinement region {}, section {}\n"
.format(mr_obj.Label, bi))
try:
shape = CfdTools.makeShapeFromReferences(
mr_patch_refs[bi])
except RuntimeError as re:
raise RuntimeError(
"Error processing mesh refinement region {}: {}"
.format(mr_obj.Label, str(re)))
if shape:
writeSurfaceMeshFromShape(shape,
self.triSurfaceDir,
mr_patch_name,
self.mesh_obj)
refinement_level = CfdTools.relLenToRefinementLevel(
mr_obj.RelativeLength)
if self.mesh_obj.MeshUtility == 'cfMesh':
if not Internal:
cf_settings['MeshRegions'][mr_patch_name] = {
'RefinementLevel':
refinement_level,
'RefinementThickness':
self.scale * Units.Quantity(
mr_obj.RefinementThickness).Value,
}
else:
cf_settings['InternalRegions'][mr_obj.Name] = {
'RefinementLevel':
refinement_level,
'RelativeLength':
mr_rellen * self.clmax * self.scale
}
elif self.mesh_obj.MeshUtility == 'snappyHexMesh':
if not Internal:
edge_level = CfdTools.relLenToRefinementLevel(
mr_obj.RegionEdgeRefinement)
snappy_settings['MeshRegions'][
mr_patch_name] = {
'RefinementLevel':
refinement_level,
'EdgeRefinementLevel':
edge_level,
'MaxRefinementLevel':
max(refinement_level, edge_level),
'Baffle':
False
}
else:
snappy_settings['InternalRegions'][
mr_patch_name] = {
'RefinementLevel': refinement_level
}
# In addition, for cfMesh and SnappyHesMesh, record matched boundary layer patches
if (self.mesh_obj.MeshUtility == 'cfMesh' or self.mesh_obj.MeshUtility == 'snappyHexMesh') \
and mr_obj.NumberLayers > 0 and not Internal and not mr_obj.Extrusion:
for k in range(len(self.patch_faces)):
if len(self.patch_faces[k][mr_id + 1]):
# Limit expansion ratio to greater than 1.0 and less than 1.2
expratio = mr_obj.ExpansionRatio
expratio = min(1.2, max(1.0, expratio))
if self.mesh_obj.MeshUtility == 'cfMesh':
cf_settings['BoundaryLayers'][self.patch_names[k][mr_id + 1]] = \
{
'NumberLayers': mr_obj.NumberLayers,
'ExpansionRatio': expratio,
'FirstLayerHeight': self.scale * Units.Quantity(mr_obj.FirstLayerHeight).Value
}
elif self.mesh_obj.MeshUtility == 'snappyHexMesh':
snappy_settings['BoundaryLayers'][self.patch_names[k][mr_id + 1]] = \
{
'NumberLayers': mr_obj.NumberLayers,
'ExpansionRatio': expratio,
# 'FinalLayerHeight': self.scale * Units.Quantity(mr_obj.FinalLayerHeight).Value
}
def parse(pathobj):
# pylint: disable=global-statement
global PRECISION
global UNIT_FORMAT
global UNIT_SPEED_FORMAT
out = ""
lastcommand = None
precision_string = '.' + str(PRECISION) + 'f'
# params = ['X','Y','Z','A','B','I','J','K','F','S'] #This list control the order of parameters
params = ['X', 'Y', 'Z', 'A', 'B', 'I', 'J', 'F', 'S', 'T', 'Q', 'R', 'L']
if hasattr(pathobj, "Group"): # We have a compound or project.
if OUTPUT_COMMENTS:
out += linenumber() + "(compound: " + pathobj.Label + ")\n"
for p in pathobj.Group:
out += parse(p)
return out
else: # parsing simple path
if not hasattr(
pathobj,
"Path"): # groups might contain non-path things like stock.
return out
if OUTPUT_COMMENTS:
out += linenumber() + "(Path: " + pathobj.Label + ")\n"
for c in pathobj.Path.Commands:
outstring = []
command = c.Name
outstring.append(command)
# if modal: only print the command if it is not the same as the last one
if MODAL is True:
if command == lastcommand:
outstring.pop(0)
# Now add the remaining parameters in order
for param in params:
if param in c.Parameters:
if param == 'F':
speed = Units.Quantity(c.Parameters['F'],
FreeCAD.Units.Velocity)
if speed.getValueAs(UNIT_SPEED_FORMAT) > 0.0:
outstring.append(param + format(
float(speed.getValueAs(UNIT_SPEED_FORMAT)),
precision_string))
elif param == 'S':
outstring.append(
param +
format(c.Parameters[param], precision_string))
elif param == 'T':
outstring.append(
param +
format(c.Parameters['T'], precision_string))
else:
pos = Units.Quantity(c.Parameters[param],
FreeCAD.Units.Length)
outstring.append(
param + format(float(pos.getValueAs(UNIT_FORMAT)),
precision_string))
# store the latest command
lastcommand = command
# Check for Tool Change:
if command == 'M6':
if OUTPUT_COMMENTS:
out += linenumber() + "(begin toolchange)\n"
for line in TOOL_CHANGE.splitlines(True):
out += linenumber() + line
if command == "message":
if OUTPUT_COMMENTS is False:
out = []
else:
outstring.pop(0) # remove the command
# prepend a line number and append a newline
if len(outstring) >= 1:
if OUTPUT_LINE_NUMBERS:
outstring.insert(0, (linenumber()))
# append the line to the final output
for w in outstring:
out += w + COMMAND_SPACE
out = out.strip() + "\n"
return out
def DVBalloonTest():
path = os.path.dirname(os.path.abspath(__file__))
print('TDBalloon path: ' + path)
templateFileSpec = path + '/TestTemplate.svg'
FreeCAD.newDocument("TDBalloon")
FreeCAD.setActiveDocument("TDBalloon")
FreeCAD.ActiveDocument = FreeCAD.getDocument("TDBalloon")
#make source feature
box = FreeCAD.ActiveDocument.addObject("Part::Box", "Box")
sphere = FreeCAD.ActiveDocument.addObject("Part::Sphere", "Sphere")
#make a page
page = FreeCAD.ActiveDocument.addObject('TechDraw::DrawPage', 'Page')
FreeCAD.ActiveDocument.addObject('TechDraw::DrawSVGTemplate', 'Template')
FreeCAD.ActiveDocument.Template.Template = templateFileSpec
FreeCAD.ActiveDocument.Page.Template = FreeCAD.ActiveDocument.Template
page.Scale = 5.0
# page.ViewObject.show() # unit tests run in console mode
#make Views
view1 = FreeCAD.ActiveDocument.addObject('TechDraw::DrawViewPart', 'View')
FreeCAD.ActiveDocument.View.Source = [FreeCAD.ActiveDocument.Box]
rc = page.addView(view1)
view1.X = Units.Quantity(30.0, Units.Length)
view1.Y = Units.Quantity(150.0, Units.Length)
view2 = FreeCAD.activeDocument().addObject('TechDraw::DrawViewPart',
'View001')
FreeCAD.activeDocument().View001.Source = [FreeCAD.activeDocument().Sphere]
rc = page.addView(view2)
view2.X = Units.Quantity(220.0, Units.Length)
view2.Y = Units.Quantity(150.0, Units.Length)
FreeCAD.ActiveDocument.recompute()
print("Place balloon")
balloon1 = FreeCAD.ActiveDocument.addObject('TechDraw::DrawViewBalloon',
'Balloon1')
balloon1.SourceView = view1
balloon1.OriginIsSet = 1
balloon1.OriginX = view1.X + Units.Quantity(20.0, Units.Length)
balloon1.OriginY = view1.Y + Units.Quantity(20.0, Units.Length)
balloon1.Text = "1"
balloon1.Y = balloon1.OriginX + Units.Quantity(20.0, Units.Length)
balloon1.X = balloon1.OriginY + Units.Quantity(20.0, Units.Length)
print("adding balloon1 to page")
rc = page.addView(balloon1)
balloon2 = FreeCAD.ActiveDocument.addObject('TechDraw::DrawViewBalloon',
'Balloon2')
balloon2.SourceView = view2
balloon2.OriginIsSet = 1
balloon2.OriginX = view2.X + Units.Quantity(20.0, Units.Length)
balloon2.OriginY = view2.Y + Units.Quantity(20.0, Units.Length)
balloon2.Text = "2"
balloon2.Y = balloon2.OriginX + Units.Quantity(20.0, Units.Length)
balloon2.X = balloon2.OriginY + Units.Quantity(20.0, Units.Length)
print("adding balloon2 to page")
rc = page.addView(balloon2)
FreeCAD.ActiveDocument.recompute()
rc = False
if ("Up-to-date" in balloon2.State) and ("Up-to-date" in balloon2.State):
rc = True
FreeCAD.closeDocument("TDBalloon")
return rc
def action(self, arg):
"""Handle the 3D scene events.
This is installed as an EventCallback in the Inventor view.
Parameters
----------
arg: dict
Dictionary with strings that indicates the type of event received
from the 3D view.
"""
import DraftGeomUtils
plane = App.DraftWorkingPlane
if arg["Type"] == "SoKeyboardEvent":
if arg["Key"] == "ESCAPE":
self.finish()
elif arg["Type"] == "SoLocation2Event": # mouse movement detection
self.point, ctrlPoint, info = gui_tool_utils.getPoint(self, arg)
# this is to make sure radius is what you see on screen
if self.center and DraftVecUtils.dist(self.point, self.center) > 0:
viewdelta = DraftVecUtils.project(self.point.sub(self.center),
plane.axis)
if not DraftVecUtils.isNull(viewdelta):
self.point = self.point.add(viewdelta.negative())
if self.step == 0: # choose center
if gui_tool_utils.hasMod(arg, gui_tool_utils.MODALT):
if not self.altdown:
self.altdown = True
self.ui.switchUi(True)
else:
if self.altdown:
self.altdown = False
self.ui.switchUi(False)
elif self.step == 1: # choose radius
if len(self.tangents) == 2:
cir = DraftGeomUtils.circleFrom2tan1pt(
self.tangents[0], self.tangents[1], self.point)
_c = DraftGeomUtils.findClosestCircle(self.point, cir)
self.center = _c.Center
self.arctrack.setCenter(self.center)
elif self.tangents and self.tanpoints:
cir = DraftGeomUtils.circleFrom1tan2pt(
self.tangents[0], self.tanpoints[0], self.point)
_c = DraftGeomUtils.findClosestCircle(self.point, cir)
self.center = _c.Center
self.arctrack.setCenter(self.center)
if gui_tool_utils.hasMod(arg, gui_tool_utils.MODALT):
if not self.altdown:
self.altdown = True
if info:
ob = self.doc.getObject(info['Object'])
num = int(info['Component'].lstrip('Edge')) - 1
ed = ob.Shape.Edges[num]
if len(self.tangents) == 2:
cir = DraftGeomUtils.circleFrom3tan(
self.tangents[0], self.tangents[1], ed)
cl = DraftGeomUtils.findClosestCircle(
self.point, cir)
self.center = cl.Center
self.rad = cl.Radius
self.arctrack.setCenter(self.center)
else:
self.rad = self.center.add(
DraftGeomUtils.findDistance(
self.center, ed).sub(self.center)).Length
else:
self.rad = DraftVecUtils.dist(self.point, self.center)
else:
if self.altdown:
self.altdown = False
self.rad = DraftVecUtils.dist(self.point, self.center)
self.ui.setRadiusValue(self.rad, "Length")
self.arctrack.setRadius(self.rad)
self.linetrack.p1(self.center)
self.linetrack.p2(self.point)
self.linetrack.on()
elif (self.step == 2): # choose first angle
currentrad = DraftVecUtils.dist(self.point, self.center)
if currentrad != 0:
angle = DraftVecUtils.angle(plane.u,
self.point.sub(self.center),
plane.axis)
else:
angle = 0
self.linetrack.p2(
DraftVecUtils.scaleTo(self.point.sub(self.center),
self.rad).add(self.center))
self.ui.setRadiusValue(math.degrees(angle), unit="Angle")
self.firstangle = angle
else:
# choose second angle
currentrad = DraftVecUtils.dist(self.point, self.center)
if currentrad != 0:
angle = DraftVecUtils.angle(plane.u,
self.point.sub(self.center),
plane.axis)
else:
angle = 0
self.linetrack.p2(
DraftVecUtils.scaleTo(self.point.sub(self.center),
self.rad).add(self.center))
self.updateAngle(angle)
self.ui.setRadiusValue(math.degrees(self.angle), unit="Angle")
self.arctrack.setApertureAngle(self.angle)
gui_tool_utils.redraw3DView()
elif arg["Type"] == "SoMouseButtonEvent": # mouse click
if arg["State"] == "DOWN" and arg["Button"] == "BUTTON1":
if self.point:
if self.step == 0: # choose center
if not self.support:
gui_tool_utils.getSupport(arg)
(self.point, ctrlPoint,
info) = gui_tool_utils.getPoint(self, arg)
if gui_tool_utils.hasMod(arg, gui_tool_utils.MODALT):
snapped = self.view.getObjectInfo(
(arg["Position"][0], arg["Position"][1]))
if snapped:
ob = self.doc.getObject(snapped['Object'])
num = int(
snapped['Component'].lstrip('Edge')) - 1
ed = ob.Shape.Edges[num]
self.tangents.append(ed)
if len(self.tangents) == 2:
self.arctrack.on()
self.ui.radiusUi()
self.step = 1
self.ui.setNextFocus()
self.linetrack.on()
_msg(translate("draft", "Pick radius"))
else:
if len(self.tangents) == 1:
self.tanpoints.append(self.point)
else:
self.center = self.point
self.node = [self.point]
self.arctrack.setCenter(self.center)
self.linetrack.p1(self.center)
self.linetrack.p2(
self.view.getPoint(arg["Position"][0],
arg["Position"][1]))
self.arctrack.on()
self.ui.radiusUi()
self.step = 1
self.ui.setNextFocus()
self.linetrack.on()
_msg(translate("draft", "Pick radius"))
if self.planetrack:
self.planetrack.set(self.point)
elif self.step == 1: # choose radius
if self.closedCircle:
self.drawArc()
else:
self.ui.labelRadius.setText(
translate("draft", "Start angle"))
self.ui.radiusValue.setToolTip(
translate("draft", "Start angle"))
self.ui.radiusValue.setText(
U.Quantity(0, U.Angle).UserString)
self.linetrack.p1(self.center)
self.linetrack.on()
self.step = 2
_msg(translate("draft", "Pick start angle"))
elif self.step == 2: # choose first angle
self.ui.labelRadius.setText(
translate("draft", "Aperture angle"))
self.ui.radiusValue.setToolTip(
translate("draft", "Aperture angle"))
self.step = 3
# scale center->point vector for proper display
# u = DraftVecUtils.scaleTo(self.point.sub(self.center), self.rad) obsolete?
self.arctrack.setStartAngle(self.firstangle)
_msg(translate("draft", "Pick aperture"))
else: # choose second angle
self.step = 4
self.drawArc()
def processExtrusions(self):
""" Find and process any extrusion objects """
twoD_extrusion_objs = []
other_extrusion_objs = []
mesh_refinements = CfdTools.getMeshRefinementObjs(self.mesh_obj)
self.extrusion_settings['ExtrusionsPresent'] = False
self.extrusion_settings['ExtrudeTo2D'] = False
self.extrusion_settings['Extrude2DPlanar'] = False
for mr in mesh_refinements:
if mr.Extrusion:
self.extrusion_settings['ExtrusionsPresent'] = True
if mr.ExtrusionType == '2DPlanar' or mr.ExtrusionType == '2DWedge':
twoD_extrusion_objs.append(mr)
else:
other_extrusion_objs.append(mr)
if mr.ExtrusionType == '2DPlanar':
self.extrusion_settings['Extrude2DPlanar'] = True
if len(twoD_extrusion_objs) > 1:
raise RuntimeError(
"For 2D meshing, there must be exactly one 2D mesh extrusion object."
)
elif len(twoD_extrusion_objs) == 1:
self.extrusion_settings['ExtrudeTo2D'] = True
all_extrusion_objs = other_extrusion_objs + twoD_extrusion_objs # Ensure 2D extrusion happens last
self.extrusion_settings['Extrusions'] = []
for extrusion_obj in all_extrusion_objs:
extrusion_shape = extrusion_obj.Shape
this_extrusion_settings = {}
if len(extrusion_shape.Faces) == 0:
raise RuntimeError("Extrusion object '{}' is empty.".format(
extrusion_obj.Label))
this_extrusion_settings[
'KeepExistingMesh'] = extrusion_obj.KeepExistingMesh
if extrusion_obj.ExtrusionType == '2DPlanar' or extrusion_obj.ExtrusionType == '2DWedge':
this_extrusion_settings['KeepExistingMesh'] = False
all_faces_planar = True
for faces in extrusion_shape.Faces:
if not isinstance(faces.Surface, Part.Plane):
all_faces_planar = False
break
if not all_faces_planar:
raise RuntimeError(
"2D mesh extrusion surface must be a flat plane.")
normal = extrusion_shape.Faces[0].Surface.Axis
normal.multiply(1.0 / normal.Length)
this_extrusion_settings['Normal'] = (normal.x, normal.y, normal.z)
this_extrusion_settings[
'ExtrusionType'] = extrusion_obj.ExtrusionType
# Get the names of the faces being extruded
mri = mesh_refinements.index(extrusion_obj)
efl = []
for l, ff in enumerate(self.patch_faces):
f = ff[mri + 1]
if len(f):
efl.append(self.patch_names[l][mri + 1])
if not efl:
raise RuntimeError(
"Extrusion patch for '{}' could not be found in the shape being meshed."
.format(extrusion_obj.Label))
this_extrusion_settings['FrontFaceList'] = tuple(efl)
this_extrusion_settings['BackFace'] = efl[0] + '_back'
this_extrusion_settings[
'Distance'] = extrusion_obj.ExtrusionThickness.getValueAs('m')
this_extrusion_settings[
'Angle'] = extrusion_obj.ExtrusionAngle.getValueAs('deg')
this_extrusion_settings[
'NumLayers'] = extrusion_obj.ExtrusionLayers
this_extrusion_settings[
'ExpansionRatio'] = extrusion_obj.ExtrusionRatio
this_extrusion_settings['AxisPoint'] = \
tuple(Units.Quantity(p, Units.Length).getValueAs('m') for p in extrusion_obj.ExtrusionAxisPoint)
axis_direction = extrusion_obj.ExtrusionAxisDirection
# Flip axis if necessary to go in same direction as patch normal (otherwise negative volume cells result)
if len(extrusion_shape.Faces) > 0:
in_plane_vector = extrusion_shape.Faces[
0].CenterOfMass - extrusion_obj.ExtrusionAxisPoint
extrusion_normal = extrusion_obj.ExtrusionAxisDirection.cross(
in_plane_vector)
face_normal = extrusion_shape.Faces[0].normalAt(0.5, 0.5)
if extrusion_normal.dot(face_normal) < 0:
axis_direction = -axis_direction
this_extrusion_settings['AxisDirection'] = tuple(
d for d in axis_direction)
self.extrusion_settings['Extrusions'].append(
this_extrusion_settings)
def writeMeshCase(self):
""" Collect case settings, and finally build a runnable case. """
CfdTools.cfdMessage(
"Populating mesh dictionaries in folder {}\n".format(
self.meshCaseDir))
# cfMesh settings
if self.mesh_obj.MeshUtility == "cfMesh":
self.cf_settings['ClMax'] = self.clmax * self.scale
if len(self.cf_settings['BoundaryLayers']) > 0:
self.cf_settings['BoundaryLayerPresent'] = True
else:
self.cf_settings['BoundaryLayerPresent'] = False
if len(self.cf_settings["InternalRegions"]) > 0:
self.cf_settings['InternalRefinementRegionsPresent'] = True
else:
self.cf_settings['InternalRefinementRegionsPresent'] = False
# SnappyHexMesh settings
elif self.mesh_obj.MeshUtility == "snappyHexMesh":
bound_box = self.part_obj.Shape.BoundBox
bC = 5 # Number of background mesh buffer cells
x_min = (bound_box.XMin - bC * self.clmax) * self.scale
x_max = (bound_box.XMax + bC * self.clmax) * self.scale
y_min = (bound_box.YMin - bC * self.clmax) * self.scale
y_max = (bound_box.YMax + bC * self.clmax) * self.scale
z_min = (bound_box.ZMin - bC * self.clmax) * self.scale
z_max = (bound_box.ZMax + bC * self.clmax) * self.scale
cells_x = int(math.ceil(bound_box.XLength / self.clmax) + 2 * bC)
cells_y = int(math.ceil(bound_box.YLength / self.clmax) + 2 * bC)
cells_z = int(math.ceil(bound_box.ZLength / self.clmax) + 2 * bC)
snappy_settings = self.snappy_settings
snappy_settings['BlockMesh'] = {
"xMin": x_min,
"xMax": x_max,
"yMin": y_min,
"yMax": y_max,
"zMin": z_min,
"zMax": z_max,
"cellsX": cells_x,
"cellsY": cells_y,
"cellsZ": cells_z
}
if len(self.snappy_settings['BoundaryLayers']) > 0:
self.snappy_settings['BoundaryLayerPresent'] = True
else:
self.snappy_settings['BoundaryLayerPresent'] = False
if self.mesh_obj.ImplicitEdgeDetection:
snappy_settings['ImplicitEdgeDetection'] = True
else:
snappy_settings['ImplicitEdgeDetection'] = False
inside_x = Units.Quantity(
self.mesh_obj.PointInMesh.get('x')).Value * self.scale
inside_y = Units.Quantity(
self.mesh_obj.PointInMesh.get('y')).Value * self.scale
inside_z = Units.Quantity(
self.mesh_obj.PointInMesh.get('z')).Value * self.scale
shape_patch_names_list = []
for k in range(len(self.patch_faces)):
for j in range(len(self.patch_faces[k])):
if len(self.patch_faces[k][j]):
shape_patch_names_list.append(self.patch_names[k][j])
snappy_settings['ShapePatchNames'] = tuple(shape_patch_names_list)
snappy_settings[
'EdgeRefinementLevel'] = CfdTools.relLenToRefinementLevel(
self.mesh_obj.EdgeRefinement)
snappy_settings['PointInMesh'] = \
{
"x": inside_x,
"y": inside_y,
"z": inside_z
}
snappy_settings[
'CellsBetweenLevels'] = self.mesh_obj.CellsBetweenLevels
if len(self.snappy_settings["InternalRegions"]) > 0:
self.snappy_settings['InternalRefinementRegionsPresent'] = True
else:
self.snappy_settings[
'InternalRefinementRegionsPresent'] = False
# GMSH settings
elif self.mesh_obj.MeshUtility == "gmsh":
exe = CfdTools.getGmshExecutable()
self.gmsh_settings['Executable'] = CfdTools.translatePath(exe)
self.gmsh_settings['HasLengthMap'] = False
if self.ele_length_map:
self.gmsh_settings['HasLengthMap'] = True
self.gmsh_settings['LengthMap'] = self.ele_length_map
self.gmsh_settings['NodeMap'] = {}
for e in self.ele_length_map:
ele_nodes = (''.join(
(str(n + 1) + ', ')
for n in self.ele_node_map[e])).rstrip(', ')
self.gmsh_settings['NodeMap'][e] = ele_nodes
self.gmsh_settings['ClMax'] = self.clmax
self.gmsh_settings['ClMin'] = self.clmin
sols = (''.join(
(str(n + 1) + ', ')
for n in range(len(self.mesh_obj.Part.Shape.Solids)))
).rstrip(', ')
self.gmsh_settings['Solids'] = sols
self.gmsh_settings['BoundaryFaceMap'] = {}
for k in range(len(self.patch_faces)):
for l in range(len(self.patch_faces[k])):
patch_faces = self.patch_faces[k][l]
patch_name = self.patch_names[k][l]
if len(patch_faces):
self.gmsh_settings['BoundaryFaceMap'][
patch_name] = ', '.join(
str(fi + 1) for fi in patch_faces)
# Perform initialisation here rather than __init__ in case of path changes
self.template_path = os.path.join(CfdTools.getModulePath(), "Data",
"Templates", "mesh")
mesh_region_present = False
if self.mesh_obj.MeshUtility == "cfMesh" and len(self.cf_settings['MeshRegions']) > 0 or \
self.mesh_obj.MeshUtility == "snappyHexMesh" and len(self.snappy_settings['MeshRegions']) > 0:
mesh_region_present = True
self.settings = {
'Name': self.part_obj.Name,
'MeshPath': self.meshCaseDir,
'FoamRuntime': CfdTools.getFoamRuntime(),
'MeshUtility': self.mesh_obj.MeshUtility,
'MeshRegionPresent': mesh_region_present,
'CfSettings': self.cf_settings,
'SnappySettings': self.snappy_settings,
'GmshSettings': self.gmsh_settings,
'ExtrusionSettings': self.extrusion_settings,
'ConvertToDualMesh': self.mesh_obj.ConvertToDualMesh
}
if CfdTools.getFoamRuntime() != 'WindowsDocker':
self.settings['TranslatedFoamPath'] = CfdTools.translatePath(
CfdTools.getFoamDir())
if self.mesh_obj.NumberOfProcesses <= 1:
self.settings['ParallelMesh'] = False
self.settings['NumberOfProcesses'] = 1
else:
self.settings['ParallelMesh'] = True
self.settings[
'NumberOfProcesses'] = self.mesh_obj.NumberOfProcesses
self.settings['NumberOfThreads'] = self.mesh_obj.NumberOfThreads
TemplateBuilder(self.meshCaseDir, self.template_path, self.settings)
# Update Allmesh permission - will fail silently on Windows
fname = os.path.join(self.meshCaseDir, "Allmesh")
import stat
s = os.stat(fname)
os.chmod(fname, s.st_mode | stat.S_IEXEC)
self.analysis.NeedsMeshRewrite = False
CfdTools.cfdMessage(
"Successfully wrote meshCase to folder {}\n".format(
self.meshCaseDir))
def writeMeshCase(self):
""" Collect case settings, and finally build a runnable case. """
CfdTools.cfdMessage(
"Populating mesh dictionaries in folder {}\n".format(
self.meshCaseDir))
if self.mesh_obj.MeshUtility == "cfMesh":
self.cf_settings['ClMax'] = self.clmax * self.scale
if len(self.cf_settings['BoundaryLayers']) > 0:
self.cf_settings['BoundaryLayerPresent'] = True
else:
self.cf_settings['BoundaryLayerPresent'] = False
if len(self.cf_settings["InternalRegions"]) > 0:
self.cf_settings['InternalRefinementRegionsPresent'] = True
else:
self.cf_settings['InternalRefinementRegionsPresent'] = False
elif self.mesh_obj.MeshUtility == "snappyHexMesh":
bound_box = self.part_obj.Shape.BoundBox
bC = 5 # Number of background mesh buffer cells
x_min = (bound_box.XMin - bC * self.clmax) * self.scale
x_max = (bound_box.XMax + bC * self.clmax) * self.scale
y_min = (bound_box.YMin - bC * self.clmax) * self.scale
y_max = (bound_box.YMax + bC * self.clmax) * self.scale
z_min = (bound_box.ZMin - bC * self.clmax) * self.scale
z_max = (bound_box.ZMax + bC * self.clmax) * self.scale
cells_x = int(math.ceil(bound_box.XLength / self.clmax) + 2 * bC)
cells_y = int(math.ceil(bound_box.YLength / self.clmax) + 2 * bC)
cells_z = int(math.ceil(bound_box.ZLength / self.clmax) + 2 * bC)
snappy_settings = self.snappy_settings
snappy_settings['BlockMesh'] = {
"xMin": x_min,
"xMax": x_max,
"yMin": y_min,
"yMax": y_max,
"zMin": z_min,
"zMax": z_max,
"cellsX": cells_x,
"cellsY": cells_y,
"cellsZ": cells_z
}
inside_x = Units.Quantity(
self.mesh_obj.PointInMesh.get('x')).Value * self.scale
inside_y = Units.Quantity(
self.mesh_obj.PointInMesh.get('y')).Value * self.scale
inside_z = Units.Quantity(
self.mesh_obj.PointInMesh.get('z')).Value * self.scale
shape_face_names_list = []
for i in self.mesh_obj.ShapeFaceNames:
shape_face_names_list.append(i)
snappy_settings['ShapeFaceNames'] = tuple(shape_face_names_list)
snappy_settings[
'EdgeRefinementLevel'] = CfdTools.relLenToRefinementLevel(
self.mesh_obj.EdgeRefinement)
snappy_settings['PointInMesh'] = {
"x": inside_x,
"y": inside_y,
"z": inside_z
}
snappy_settings[
'CellsBetweenLevels'] = self.mesh_obj.CellsBetweenLevels
if self.mesh_obj.NumberCores <= 1:
self.mesh_obj.NumberCores = 1
snappy_settings['ParallelMesh'] = False
else:
snappy_settings['ParallelMesh'] = True
snappy_settings['NumberCores'] = self.mesh_obj.NumberCores
if len(self.snappy_settings["InternalRegions"]) > 0:
self.snappy_settings['InternalRefinementRegionsPresent'] = True
else:
self.snappy_settings[
'InternalRefinementRegionsPresent'] = False
elif self.mesh_obj.MeshUtility == "gmsh":
if platform.system() == "Windows":
exe = os.path.join(FreeCAD.getHomePath(), 'bin', 'gmsh.exe')
else:
exe = subprocess.check_output(
["which", "gmsh"], universal_newlines=True).rstrip('\n')
self.gmsh_settings['Executable'] = CfdTools.translatePath(exe)
self.gmsh_settings['ShapeFile'] = self.temp_file_shape
self.gmsh_settings['HasLengthMap'] = False
if self.ele_length_map:
self.gmsh_settings['HasLengthMap'] = True
self.gmsh_settings['LengthMap'] = self.ele_length_map
self.gmsh_settings['NodeMap'] = {}
for e in self.ele_length_map:
ele_nodes = (''.join(
(str(n + 1) + ', ')
for n in self.ele_node_map[e])).rstrip(', ')
self.gmsh_settings['NodeMap'][e] = ele_nodes
self.gmsh_settings['ClMax'] = self.clmax
self.gmsh_settings['ClMin'] = self.clmin
sols = (''.join(
(str(n + 1) + ', ')
for n in range(len(self.mesh_obj.Part.Shape.Solids)))
).rstrip(', ')
self.gmsh_settings['Solids'] = sols
self.gmsh_settings['BoundaryFaceMap'] = {}
# Write one boundary per face
for i in range(len(self.mesh_obj.Part.Shape.Faces)):
self.gmsh_settings['BoundaryFaceMap']['face' + str(i)] = i + 1
self.gmsh_settings['MeshFile'] = self.temp_file_mesh
# Perform initialisation here rather than __init__ in case of path changes
self.template_path = os.path.join(CfdTools.get_module_path(), "data",
"defaultsMesh")
mesh_region_present = False
if self.mesh_obj.MeshUtility == "cfMesh" and len(self.cf_settings['MeshRegions']) > 0 or \
self.mesh_obj.MeshUtility == "snappyHexMesh" and len(self.snappy_settings['MeshRegions']) > 0:
mesh_region_present = True
self.settings = {
'Name': self.part_obj.Name,
'MeshPath': self.meshCaseDir,
'FoamRuntime': CfdTools.getFoamRuntime(),
'TranslatedFoamPath':
CfdTools.translatePath(CfdTools.getFoamDir()),
'MeshUtility': self.mesh_obj.MeshUtility,
'MeshRegionPresent': mesh_region_present,
'CfSettings': self.cf_settings,
'SnappySettings': self.snappy_settings,
'GmshSettings': self.gmsh_settings,
'TwoDSettings': self.two_d_settings
}
TemplateBuilder.TemplateBuilder(self.meshCaseDir, self.template_path,
self.settings)
# Update Allmesh permission - will fail silently on Windows
fname = os.path.join(self.meshCaseDir, "Allmesh")
import stat
s = os.stat(fname)
os.chmod(fname, s.st_mode | stat.S_IEXEC)
CfdTools.cfdMessage(
"Successfully wrote meshCase to folder {}\n".format(
self.meshCaseDir))
def parse(pathobj):
global DRILL_RETRACT_MODE
global MOTION_MODE
global CURRENT_X
global CURRENT_Y
global CURRENT_Z
out = ''
lastcommand = None
precision_string = '.' + str(PRECISION) + 'f'
params = [
'X', 'Y', 'Z', 'A', 'B', 'C', 'U', 'V', 'W', 'I', 'J', 'K', 'F', 'S',
'T', 'Q', 'R', 'L', 'P'
]
if hasattr(pathobj, 'Group'): # We have a compound or project.
if OUTPUT_COMMENTS:
out += linenumber() + '(Compound: ' + pathobj.Label + ')\n'
for p in pathobj.Group:
out += parse(p)
return out
else: # Parsing simple path
# groups might contain non-path things like stock.
if not hasattr(pathobj, 'Path'):
return out
if OUTPUT_COMMENTS and OUTPUT_PATH:
out += linenumber() + '(Path: ' + pathobj.Label + ')\n'
for c in pathobj.Path.Commands:
outlist = []
command = c.Name
outlist.append(command)
# Debug:
# print('pathobj.Path.Commands:', c)
# If modal is True, delete duplicate commands:
if MODAL:
if command == lastcommand:
outlist.pop(0)
# Add the remaining parameters in order:
for param in params:
if param in c.Parameters:
if param == 'F':
if command not in RAPID_MOVES:
feedRate = Units.Quantity(c.Parameters['F'],
FreeCAD.Units.Velocity)
if feedRate.getValueAs(UNIT_FEED_FORMAT) > 0.0:
outlist.append(param + format(
float(feedRate.getValueAs(
UNIT_FEED_FORMAT)), precision_string))
elif param == 'T':
outlist.append(param + str(int(c.Parameters[param])))
elif param in ['H', 'D', 'S', 'P', 'L']:
outlist.append(param + str(c.Parameters[param]))
elif param in ['A', 'B', 'C']:
outlist.append(
param +
format(c.Parameters[param], precision_string))
# [X, Y, Z, U, V, W, I, J, K, R, Q]
else:
pos = Units.Quantity(c.Parameters[param],
FreeCAD.Units.Length)
outlist.append(
param + format(float(pos.getValueAs(UNIT_FORMAT)),
precision_string))
# Store the latest command:
lastcommand = command
# Capture the current position for subsequent calculations:
if command in MOTION_COMMANDS:
if 'X' in c.Parameters:
CURRENT_X = Units.Quantity(c.Parameters['X'],
FreeCAD.Units.Length)
if 'Y' in c.Parameters:
CURRENT_Y = Units.Quantity(c.Parameters['Y'],
FreeCAD.Units.Length)
if 'Z' in c.Parameters:
CURRENT_Z = Units.Quantity(c.Parameters['Z'],
FreeCAD.Units.Length)
if command in ('G98', 'G99'):
DRILL_RETRACT_MODE = command
if TRANSLATE_DRILL_CYCLES:
if command in ('G81', 'G82', 'G83'):
out += drill_translate(outlist, command, c.Parameters)
# Erase the line just translated:
outlist = []
if SPINDLE_WAIT > 0:
if command in ('M3', 'M03', 'M4', 'M04'):
out += linenumber() + format_outlist(outlist) + '\n'
# RRF: P for milliseconds, S for seconds, change P to S
out += linenumber()
out += format_outlist(['G4', 'S%s' % SPINDLE_WAIT])
out += '\n'
outlist = []
# Check for Tool Change:
if command in ('M6', 'M06'):
if OUTPUT_COMMENTS:
out += linenumber() + '(Begin toolchange)\n'
if OUTPUT_TOOL_CHANGE:
for line in TOOL_CHANGE.splitlines(True):
out += linenumber() + line + '\n'
outlist[0] = ' '
outlist[-1] = ('T' + str(int(c.Parameters['T'])))
if not OUTPUT_TOOL_CHANGE and OUTPUT_COMMENTS:
# next 2 lines could also be replaced by a single line as "outlist = []"
outlist[0] = ' '
outlist[-1] = ' '
if not OUTPUT_TOOL_CHANGE and not OUTPUT_COMMENTS:
outlist = []
if command == 'message':
if OUTPUT_COMMENTS:
outlist.pop(0) # remove the command
else:
out = []
if command in SUPPRESS_COMMANDS:
outlist[0] = '(' + outlist[0]
outlist[-1] = outlist[-1] + ')'
# Remove embedded comments:
if not OUTPUT_COMMENTS:
tmplist = []
list_index = 0
while list_index < len(outlist):
left_index = outlist[list_index].find('(')
if left_index == -1: # Not a comment
tmplist.append(outlist[list_index])
else: # This line contains a comment, and possibly more
right_index = outlist[list_index].find(')')
comment_area = outlist[list_index][
left_index:right_index + 1]
line_minus_comment = outlist[list_index].replace(
comment_area, '').strip()
if line_minus_comment:
# Line contained more than just a comment
tmplist.append(line_minus_comment)
list_index += 1
# Done removing comments
outlist = tmplist
# Prepend a line number and append a newline
if len(outlist) >= 1:
out += linenumber() + format_outlist(outlist) + '\n'
return out
def parse(pathobj):
out = ""
lastcommand = None
precision_string = '.' + str(PRECISION) + 'f'
currLocation = {} # keep track for no doubles
# The params list control the order of parameters
params = [
'X', 'Y', 'Z', 'A', 'B', 'C', 'I', 'J', 'K', 'R', 'F', 'S', 'T', 'H',
'L', 'Q'
]
firstmove = Path.Command("G0", {"X": -1, "Y": -1, "Z": -1, "F": 0.0})
currLocation.update(firstmove.Parameters) # set First location Parameters
if hasattr(pathobj, "Group"):
# We have a compound or project.
# if OUTPUT_COMMENTS:
# out += linenumber() + "(compound: " + pathobj.Label + ")\n"
for p in pathobj.Group:
out += parse(p)
return out
else:
# parsing simple path
# groups might contain non-path things like stock.
if not hasattr(pathobj, "Path"):
return out
# if OUTPUT_COMMENTS:
# out += linenumber() + "(" + pathobj.Label + ")\n"
for c in pathobj.Path.Commands:
commandlist = [
] # list of elements in the command, code and params.
command = c.Name.strip() # command M or G code or comment string
commandlist.append(command)
# if modal: only print the command if it is not the same as the last one
if MODAL is True:
if command == lastcommand:
commandlist.pop(0)
if c.Name[0] == '(' and not OUTPUT_COMMENTS: # command is a comment
continue
# Now add the remaining parameters in order
for param in params:
if param in c.Parameters:
if param == 'F' and (
currLocation[param] != c.Parameters[param]
or REPEAT_ARGUMENTS):
if c.Name not in ["G0", "G00"]: # No F in G0
speed = Units.Quantity(c.Parameters['F'],
FreeCAD.Units.Velocity)
if speed.getValueAs(UNIT_SPEED_FORMAT) > 0.0:
commandlist.append(param + format(
float(speed.getValueAs(UNIT_SPEED_FORMAT)),
precision_string))
else:
continue
elif param == 'T':
commandlist.append(param + str(int(c.Parameters['T'])))
elif param == 'H':
commandlist.append(param + str(int(c.Parameters['H'])))
elif param == 'D':
commandlist.append(param + str(int(c.Parameters['D'])))
elif param == 'S':
commandlist.append(param + str(int(c.Parameters['S'])))
else:
if (not REPEAT_ARGUMENTS) and (
param
in currLocation) and (currLocation[param]
== c.Parameters[param]):
continue
else:
pos = Units.Quantity(c.Parameters[param],
FreeCAD.Units.Length)
commandlist.append(
param +
format(float(pos.getValueAs(UNIT_FORMAT)),
precision_string))
# store the latest command
lastcommand = command
currLocation.update(c.Parameters)
# Check for Tool Change:
if command == 'M6':
for line in TOOL_CHANGE.splitlines(True):
out += linenumber() + line
# add height offset
if USE_TLO:
tool_height = '\nG43 H' + str(int(c.Parameters['T']))
commandlist.append(tool_height)
if command == "message":
if OUTPUT_COMMENTS is False:
out = []
else:
commandlist.pop(0) # remove the command
# prepend a line number and append a newline
if len(commandlist) >= 1:
if OUTPUT_LINE_NUMBERS:
commandlist.insert(0, (linenumber()))
# append the line to the final output
for w in commandlist:
out += w.strip() + COMMAND_SPACE
if (trace_gcode):
print("parse : >>{}".format(out))
out = out.strip() + "\n"
return out
def drill_translate(outlist, cmd, params):
global DRILL_RETRACT_MODE
global MOTION_MODE
global CURRENT_X
global CURRENT_Y
global CURRENT_Z
global UNITS
global UNIT_FORMAT
global UNIT_FEED_FORMAT
class Drill: # Using a class is necessary for the nested functions.
gcode = ''
strFormat = '.' + str(PRECISION) + 'f'
if OUTPUT_COMMENTS: # Comment the original command
outlist[0] = '(' + outlist[0]
outlist[-1] = outlist[-1] + ')'
Drill.gcode += linenumber() + format_outlist(outlist) + '\n'
# Cycle conversion only converts the cycles in the XY plane (G17).
# --> ZX (G18) and YZ (G19) planes produce false gcode.
drill_X = Units.Quantity(params['X'], FreeCAD.Units.Length)
drill_Y = Units.Quantity(params['Y'], FreeCAD.Units.Length)
drill_Z = Units.Quantity(params['Z'], FreeCAD.Units.Length)
drill_R = Units.Quantity(params['R'], FreeCAD.Units.Length)
drill_F = Units.Quantity(params['F'], FreeCAD.Units.Velocity)
if cmd == 'G82':
drill_DwellTime = params['P']
elif cmd == 'G83':
drill_Step = Units.Quantity(params['Q'], FreeCAD.Units.Length)
# R less than Z is error
if drill_R < drill_Z:
Drill.gcode += linenumber() + '(drill cycle error: R less than Z )\n'
return Drill.gcode
# Z height to retract to when drill cycle is done:
if DRILL_RETRACT_MODE == 'G98' and CURRENT_Z > drill_R:
RETRACT_Z = CURRENT_Z
else:
RETRACT_Z = drill_R
# Z motion nested functions:
def rapid_Z_to(new_Z):
Drill.gcode += linenumber() + 'G0 Z'
Drill.gcode += format(float(new_Z.getValueAs(UNIT_FORMAT)),
strFormat) + '\n'
def feed_Z_to(new_Z):
Drill.gcode += linenumber() + 'G1 Z'
Drill.gcode += format(float(new_Z.getValueAs(UNIT_FORMAT)),
strFormat) + ' F'
Drill.gcode += format(float(drill_F.getValueAs(UNIT_FEED_FORMAT)),
'.2f') + '\n'
# Make sure that Z is not below RETRACT_Z:
if CURRENT_Z < RETRACT_Z:
rapid_Z_to(RETRACT_Z)
# Rapid to hole position XY:
Drill.gcode += linenumber() + 'G0 X'
Drill.gcode += format(float(drill_X.getValueAs(UNIT_FORMAT)),
strFormat) + ' Y'
Drill.gcode += format(float(drill_Y.getValueAs(UNIT_FORMAT)),
strFormat) + '\n'
# Rapid to R:
rapid_Z_to(drill_R)
# *************************************************************************
# * Drill cycles: *
# * G80 Cancel the drill cycle *
# * G81 Drill full depth in one pass *
# * G82 Drill full depth in one pass, and pause at the bottom *
# * G83 Drill in pecks, raising the drill to R height after each peck *
# * In preparation for a rapid to the next hole position: *
# * G98 After the hole has been drilled, retract to the initial Z value *
# * G99 After the hole has been drilled, retract to R height *
# * Select G99 only if safe to move from hole to hole at the R height *
# *************************************************************************
if cmd in ('G81', 'G82'):
feed_Z_to(drill_Z) # Drill hole in one step
if cmd == 'G82': # Dwell time delay at the bottom of the hole
Drill.gcode += linenumber() + 'G4 S' + str(drill_DwellTime) + '\n'
# RRF uses P for milliseconds, S for seconds, change P to S
elif cmd == 'G83': # Peck drill cycle:
chip_Space = drill_Step * 0.5
next_Stop_Z = drill_R - drill_Step
while next_Stop_Z >= drill_Z:
feed_Z_to(next_Stop_Z) # Drill one peck of depth
# Set next depth, next_Stop_Z is still at the current hole depth
if (next_Stop_Z - drill_Step) >= drill_Z:
# Rapid up to clear chips:
rapid_Z_to(drill_R)
# Rapid down to just above last peck depth:
rapid_Z_to(next_Stop_Z + chip_Space)
# Update next_Stop_Z to next depth:
next_Stop_Z -= drill_Step
elif next_Stop_Z == drill_Z:
break # Done
else: # More to drill, but less than drill_Step
# Rapid up to clear chips:
rapid_Z_to(drill_R)
# Rapid down to just above last peck depth:
rapid_Z_to(next_Stop_Z + chip_Space)
# Dril remainder of the hole depth:
feed_Z_to(drill_Z)
break # Done
rapid_Z_to(RETRACT_Z) # Done, retract the drill
return Drill.gcode
def check_prerequisites(self):
from FreeCAD import Units
message = ""
# analysis
if not self.analysis:
message += "No active Analysis\n"
if self.analysis_type not in self.known_analysis_types:
message += "Unknown analysis type: {}\n".format(self.analysis_type)
if not self.working_dir:
message += "Working directory not set\n"
import os
if not (os.path.isdir(self.working_dir)):
message += "Working directory \'{}\' doesn't exist.".format(
self.working_dir)
# solver
if not self.solver:
message += "No solver object defined in the analysis\n"
else:
if self.analysis_type == "frequency":
if not hasattr(self.solver, "EigenmodeHighLimit"):
message += "Frequency analysis: Solver has no EigenmodeHighLimit.\n"
elif not hasattr(self.solver, "EigenmodeLowLimit"):
message += "Frequency analysis: Solver has no EigenmodeLowLimit.\n"
elif not hasattr(self.solver, "EigenmodesCount"):
message += "Frequency analysis: Solver has no EigenmodesCount.\n"
if hasattr(self.solver, "MaterialNonlinearity"
) and self.solver.MaterialNonlinearity == "nonlinear":
if not self.materials_nonlinear:
message += "Solver is set to nonlinear materials, but there is no nonlinear material in the analysis.\n"
if self.solver.SolverType == 'FemSolverCalculix' and self.solver.GeometricalNonlinearity != "nonlinear":
# nonlinear geometry --> should be set https://forum.freecadweb.org/viewtopic.php?f=18&t=23101&p=180489#p180489
message += "Solver CalculiX triggers nonlinear geometry for nonlinear material, thus it should to be set too.\n"
# mesh
if not self.mesh:
message += "No mesh object defined in the analysis\n"
if self.mesh:
if self.mesh.FemMesh.VolumeCount == 0 and self.mesh.FemMesh.FaceCount > 0 and not self.shell_thicknesses:
message += "FEM mesh has no volume elements, either define a shell thicknesses or provide a FEM mesh with volume elements.\n"
if self.mesh.FemMesh.VolumeCount == 0 and self.mesh.FemMesh.FaceCount == 0 and self.mesh.FemMesh.EdgeCount > 0 and not self.beam_sections and not self.fluid_sections:
message += "FEM mesh has no volume and no shell elements, either define a beam/fluid section or provide a FEM mesh with volume elements.\n"
if self.mesh.FemMesh.VolumeCount == 0 and self.mesh.FemMesh.FaceCount == 0 and self.mesh.FemMesh.EdgeCount == 0:
message += "FEM mesh has neither volume nor shell or edge elements. Provide a FEM mesh with elements!\n"
# material linear and nonlinear
if not self.materials_linear:
message += "No material object defined in the analysis\n"
has_no_references = False
for m in self.materials_linear:
if len(m['Object'].References) == 0:
if has_no_references is True:
message += "More than one material has an empty references list (Only one empty references list is allowed!).\n"
has_no_references = True
mat_ref_shty = ''
for m in self.materials_linear:
ref_shty = get_refshape_type(m['Object'])
if not mat_ref_shty:
mat_ref_shty = ref_shty
if mat_ref_shty and ref_shty and ref_shty != mat_ref_shty: # mat_ref_shty could be empty in one material, only the not empty ones should have the same shape type
message += 'Some material objects do not have the same reference shape type (all material objects must have the same reference shape type, at the moment).\n'
for m in self.materials_linear:
mat_map = m['Object'].Material
mat_obj = m['Object']
if mat_obj.Category == 'Solid':
if 'YoungsModulus' in mat_map:
# print(Units.Quantity(mat_map['YoungsModulus']).Value)
if not Units.Quantity(mat_map['YoungsModulus']).Value:
message += "Value of YoungsModulus is set to 0.0.\n"
else:
message += "No YoungsModulus defined for at least one material.\n"
if 'PoissonRatio' not in mat_map:
message += "No PoissonRatio defined for at least one material.\n" # PoissonRatio is allowed to be 0.0 (in ccx), but it should be set anyway.
if self.analysis_type == "frequency" or self.selfweight_constraints:
if 'Density' not in mat_map:
message += "No Density defined for at least one material.\n"
if self.analysis_type == "thermomech":
if 'ThermalConductivity' in mat_map:
if not Units.Quantity(
mat_map['ThermalConductivity']).Value:
message += "Value of ThermalConductivity is set to 0.0.\n"
else:
message += "Thermomechanical analysis: No ThermalConductivity defined for at least one material.\n"
if 'ThermalExpansionCoefficient' not in mat_map and mat_obj.Category == 'Solid':
message += "Thermomechanical analysis: No ThermalExpansionCoefficient defined for at least one material.\n" # allowed to be 0.0 (in ccx)
if 'SpecificHeat' not in mat_map:
message += "Thermomechanical analysis: No SpecificHeat defined for at least one material.\n" # allowed to be 0.0 (in ccx)
for m in self.materials_linear:
has_nonlinear_material = False
for nlm in self.materials_nonlinear:
if nlm['Object'].LinearBaseMaterial == m['Object']:
if has_nonlinear_material is False:
has_nonlinear_material = True
else:
message += "At least two nonlinear materials use the same linear base material. Only one nonlinear material for each linear material allowed.\n"
# which analysis needs which constraints
# no check in the regard of loads existence (constraint force, pressure, self weight) is done because an analysis without loads at all is an valid analysis too
if self.analysis_type == "static":
if not (self.fixed_constraints or self.displacement_constraints):
message += "Static analysis: Neither constraint fixed nor constraint displacement defined.\n"
if self.analysis_type == "thermomech":
if not self.initialtemperature_constraints:
if not self.fluid_sections:
message += "Thermomechanical analysis: No initial temperature defined.\n"
if len(self.initialtemperature_constraints) > 1:
message += "Thermomechanical analysis: Only one initial temperature is allowed.\n"
# constraints
# fixed
if self.fixed_constraints:
for c in self.fixed_constraints:
if len(c['Object'].References) == 0:
message += "At least one constraint fixed has an empty reference.\n"
# displacement
if self.displacement_constraints:
for di in self.displacement_constraints:
if len(di['Object'].References) == 0:
message += "At least one constraint displacement has an empty reference.\n"
# plane rotation
if self.planerotation_constraints:
for c in self.planerotation_constraints:
if len(c['Object'].References) == 0:
message += "At least one constraint plane rotation has an empty reference.\n"
# contact
if self.contact_constraints:
for c in self.contact_constraints:
if len(c['Object'].References) == 0:
message += "At least one constraint contact has an empty reference.\n"
# transform
if self.transform_constraints:
for c in self.transform_constraints:
if len(c['Object'].References) == 0:
message += "At least one constraint transform has an empty reference.\n"
# pressure
if self.pressure_constraints:
for c in self.pressure_constraints:
if len(c['Object'].References) == 0:
message += "At least one constraint pressure has an empty reference.\n"
# force
if self.force_constraints:
for c in self.force_constraints:
if len(c['Object'].References) == 0:
message += "At least one constraint force has an empty reference.\n"
# temperature
if self.temperature_constraints:
for c in self.temperature_constraints:
if len(c['Object'].References) == 0:
message += "At least one constraint temperature has an empty reference.\n"
# heat flux
if self.heatflux_constraints:
for c in self.heatflux_constraints:
if len(c['Object'].References) == 0:
message += "At least one constraint heat flux has an empty reference.\n"
# beam section
if self.beam_sections:
if self.shell_thicknesses:
# this needs to be checked only once either here or in shell_thicknesses
message += "Beam Sections and shell thicknesses in one analysis is not supported at the moment.\n"
if self.fluid_sections:
# this needs to be checked only once either here or in shell_thicknesses
message += "Beam Sections and Fluid Sections in one analysis is not supported at the moment.\n"
has_no_references = False
for b in self.beam_sections:
if len(b['Object'].References) == 0:
if has_no_references is True:
message += "More than one beam section has an empty references list (Only one empty references list is allowed!).\n"
has_no_references = True
if self.mesh:
if self.mesh.FemMesh.FaceCount > 0 or self.mesh.FemMesh.VolumeCount > 0:
message += "Beam sections defined but FEM mesh has volume or shell elements.\n"
if self.mesh.FemMesh.EdgeCount == 0:
message += "Beam sections defined but FEM mesh has no edge elements.\n"
# shell thickness
if self.shell_thicknesses:
has_no_references = False
for s in self.shell_thicknesses:
if len(s['Object'].References) == 0:
if has_no_references is True:
message += "More than one shell thickness has an empty references list (Only one empty references list is allowed!).\n"
has_no_references = True
if self.mesh:
if self.mesh.FemMesh.VolumeCount > 0:
message += "Shell thicknesses defined but FEM mesh has volume elements.\n"
if self.mesh.FemMesh.FaceCount == 0:
message += "Shell thicknesses defined but FEM mesh has no shell elements.\n"
# fluid section
if self.fluid_sections:
if not self.selfweight_constraints:
message += "A fluid network analysis requires self weight constraint to be applied"
if self.analysis_type != "thermomech":
message += "A fluid network analysis can only be done in a thermomech analysis"
has_no_references = False
for f in self.fluid_sections:
if len(f['Object'].References) == 0:
if has_no_references is True:
message += "More than one fluid section has an empty references list (Only one empty references list is allowed!).\n"
has_no_references = True
if self.mesh:
if self.mesh.FemMesh.FaceCount > 0 or self.mesh.FemMesh.VolumeCount > 0:
message += "Fluid sections defined but FEM mesh has volume or shell elements.\n"
if self.mesh.FemMesh.EdgeCount == 0:
message += "Fluid sections defined but FEM mesh has no edge elements.\n"
return message
def parse(pathobj):
global PRECISION
global MODAL
global OUTPUT_DOUBLES
global UNIT_FORMAT
global UNIT_SPEED_FORMAT
out = ""
lastcommand = None
precision_string = '.' + str(PRECISION) + 'f'
currLocation = {} # keep track for no doubles
# the order of parameters
# linuxcnc doesn't want K properties on XY plane Arcs need work.
params = [
'X', 'Y', 'Z', 'A', 'B', 'C', 'I', 'J', 'F', 'S', 'T', 'Q', 'R', 'L',
'H', 'D', 'P'
]
firstmove = Path.Command("G0", {"X": -1, "Y": -1, "Z": -1, "F": 0.0})
currLocation.update(firstmove.Parameters) # set First location Parameters
if hasattr(pathobj, "Group"): # We have a compound or project.
# if OUTPUT_COMMENTS:
# out += linenumber() + "(compound: " + pathobj.Label + ")\n"
for p in pathobj.Group:
out += parse(p)
return out
else: # parsing simple path
# groups might contain non-path things like stock.
if not hasattr(pathobj, "Path"):
return out
# if OUTPUT_COMMENTS:
# out += linenumber() + "(" + pathobj.Label + ")\n"
for c in pathobj.Path.Commands:
outstring = []
command = c.Name
outstring.append(command)
# if modal: suppress the command if it is the same as the last one
if MODAL is True:
if command == lastcommand:
outstring.pop(0)
if c.Name[0] == '(' and not OUTPUT_COMMENTS: # command is a comment
continue
# Now add the remaining parameters in order
for param in params:
if param in c.Parameters:
if param == 'F' and (
currLocation[param] != c.Parameters[param]
or OUTPUT_DOUBLES):
if c.Name not in [
"G0", "G00"
]: # linuxcnc doesn't use rapid speeds
speed = Units.Quantity(c.Parameters['F'],
FreeCAD.Units.Velocity)
if speed.getValueAs(UNIT_SPEED_FORMAT) > 0.0:
outstring.append(param + format(
float(speed.getValueAs(UNIT_SPEED_FORMAT)),
precision_string))
else:
continue
elif param == 'T':
outstring.append(param + str(int(c.Parameters['T'])))
elif param == 'H':
outstring.append(param + str(int(c.Parameters['H'])))
elif param == 'D':
outstring.append(param + str(int(c.Parameters['D'])))
elif param == 'S':
outstring.append(param + str(int(c.Parameters['S'])))
else:
if (not OUTPUT_DOUBLES) and (
param
in currLocation) and (currLocation[param]
== c.Parameters[param]):
continue
else:
pos = Units.Quantity(c.Parameters[param],
FreeCAD.Units.Length)
outstring.append(
param +
format(float(pos.getValueAs(UNIT_FORMAT)),
precision_string))
# store the latest command
lastcommand = command
currLocation.update(c.Parameters)
# Check for Tool Change:
if command == 'M6':
# if OUTPUT_COMMENTS:
# out += linenumber() + "(begin toolchange)\n"
for line in TOOL_CHANGE.splitlines(True):
out += linenumber() + line
if command == "message":
if OUTPUT_COMMENTS is False:
out = []
else:
outstring.pop(0) # remove the command
# prepend a line number and append a newline
if len(outstring) >= 1:
if OUTPUT_LINE_NUMBERS:
outstring.insert(0, (linenumber()))
# append the line to the final output
for w in outstring:
out += w + COMMAND_SPACE
out = out.strip() + "\n"
return out
def convert(quantityStr, unit):
quantity = Units.Quantity(quantityStr)
for key, setting in UNITS.items():
unit = unit.replace(key, setting)
return float(quantity.getValueAs(unit))
def __init__(self):
self.name = "Polar array"
_log(_tr("Task panel:") + " {}".format(_tr(self.name)))
# The .ui file must be loaded into an attribute
# called `self.form` so that it is displayed in the task panel.
ui_file = ":/ui/TaskPanel_PolarArray.ui"
self.form = Gui.PySideUic.loadUi(ui_file)
icon_name = "Draft_PolarArray"
svg = ":/icons/" + icon_name
pix = QtGui.QPixmap(svg)
icon = QtGui.QIcon.fromTheme(icon_name, QtGui.QIcon(svg))
self.form.setWindowIcon(icon)
self.form.setWindowTitle(_tr(self.name))
self.form.label_icon.setPixmap(pix.scaled(32, 32))
# -------------------------------------------------------------------
# Default values for the internal function,
# and for the task panel interface
start_angle = U.Quantity(360.0, App.Units.Angle)
angle_unit = start_angle.getUserPreferred()[2]
self.angle = start_angle.Value
self.number = 5
self.form.spinbox_angle.setProperty('rawValue', self.angle)
self.form.spinbox_angle.setProperty('unit', angle_unit)
self.form.spinbox_number.setValue(self.number)
start_point = U.Quantity(0.0, App.Units.Length)
length_unit = start_point.getUserPreferred()[2]
self.center = App.Vector(start_point.Value, start_point.Value,
start_point.Value)
self.form.input_c_x.setProperty('rawValue', self.center.x)
self.form.input_c_x.setProperty('unit', length_unit)
self.form.input_c_y.setProperty('rawValue', self.center.y)
self.form.input_c_y.setProperty('unit', length_unit)
self.form.input_c_z.setProperty('rawValue', self.center.z)
self.form.input_c_z.setProperty('unit', length_unit)
self.fuse = utils.get_param("Draft_array_fuse", False)
self.use_link = utils.get_param("Draft_array_Link", True)
self.form.checkbox_fuse.setChecked(self.fuse)
self.form.checkbox_link.setChecked(self.use_link)
# -------------------------------------------------------------------
# Some objects need to be selected before we can execute the function.
self.selection = None
# This is used to test the input of the internal function.
# It should be changed to True before we can execute the function.
self.valid_input = False
self.set_widget_callbacks()
self.tr_true = QT_TRANSLATE_NOOP("Draft", "True")
self.tr_false = QT_TRANSLATE_NOOP("Draft", "False")
# The mask is not used at the moment, but could be used in the future
# by a callback to restrict the coordinates of the pointer.
self.mask = ""
def __init__(self, gmsh_mesh_obj, analysis=None):
# mesh obj
self.mesh_obj = gmsh_mesh_obj
# analysis
if analysis:
self.analysis = analysis
else:
self.analysis = None
# part to mesh
self.part_obj = self.mesh_obj.Part
# clmax, CharacteristicLengthMax: float, 0.0 = 1e+22
self.clmax = Units.Quantity(
self.mesh_obj.CharacteristicLengthMax).Value
if self.clmax == 0.0:
self.clmax = 1e+22
# clmin, CharacteristicLengthMin: float
self.clmin = Units.Quantity(
self.mesh_obj.CharacteristicLengthMin).Value
# geotol, GeometryTolerance: float, 0.0 = 1e-08
self.geotol = self.mesh_obj.GeometryTolerance
if self.geotol == 0.0:
self.geotol = 1e-08
# order
# known_element_orders = ["1st", "2nd"]
self.order = self.mesh_obj.ElementOrder
if self.order == "1st":
self.order = "1"
elif self.order == "2nd":
self.order = "2"
else:
Console.PrintError("Error in order\n")
# dimension
self.dimension = self.mesh_obj.ElementDimension
# Algorithm2D
algo2D = self.mesh_obj.Algorithm2D
if algo2D == "Automatic":
self.algorithm2D = "2"
elif algo2D == "MeshAdapt":
self.algorithm2D = "1"
elif algo2D == "Delaunay":
self.algorithm2D = "5"
elif algo2D == "Frontal":
self.algorithm2D = "6"
elif algo2D == "BAMG":
self.algorithm2D = "7"
elif algo2D == "DelQuad":
self.algorithm2D = "8"
else:
self.algorithm2D = "2"
# Algorithm3D
algo3D = self.mesh_obj.Algorithm3D
if algo3D == "Automatic":
self.algorithm3D = "1"
elif algo3D == "Delaunay":
self.algorithm3D = "1"
elif algo3D == "New Delaunay":
self.algorithm3D = "2"
elif algo3D == "Frontal":
self.algorithm3D = "4"
elif algo3D == "Frontal Delaunay":
self.algorithm3D = "5"
elif algo3D == "Frontal Hex":
self.algorithm3D = "6"
elif algo3D == "MMG3D":
self.algorithm3D = "7"
elif algo3D == "R-tree":
self.algorithm3D = "9"
else:
self.algorithm3D = "1"
# mesh groups
if self.mesh_obj.GroupsOfNodes is True:
self.group_nodes_export = True
else:
self.group_nodes_export = False
self.group_elements = {}
# mesh regions
self.ele_length_map = {} # { "ElementString" : element length }
self.ele_node_map = {} # { "ElementString" : [element nodes] }
# mesh boundary layer
self.bl_setting_list = [
] # list of dict, each item map to MeshBoundaryLayer object
self.bl_boundary_list = [
] # to remove duplicated boundary edge or faces
# other initializations
self.temp_file_geometry = ""
self.temp_file_mesh = ""
self.temp_file_geo = ""
self.mesh_name = ""
self.gmsh_bin = ""
self.error = False
def onChanged(self,vobj,prop):
if prop in ["Text","Decimals","ShowUnit"]:
if hasattr(self,"text1") and hasattr(self,"text2") and hasattr(vobj,"Text"):
self.text1.string.deleteValues(0)
self.text2.string.deleteValues(0)
text1 = []
text2 = []
first = True
for t in vobj.Text:
if t:
if hasattr(vobj.Object,"Area"):
from FreeCAD import Units
q = Units.Quantity(vobj.Object.Area,Units.Area).getUserPreferred()
qt = vobj.Object.Area/q[1]
if hasattr(vobj,"Decimals"):
if vobj.Decimals == 0:
qt = str(int(qt))
else:
f = "%."+str(abs(vobj.Decimals))+"f"
qt = f % qt
else:
qt = str(qt)
if hasattr(vobj,"ShowUnit"):
if vobj.ShowUnit:
qt = qt + q[2].replace("^2",u"\xb2") # square symbol
t = t.replace("$area",qt)
t = t.replace("$label",vobj.Object.Label)
if hasattr(vobj.Object,"Tag"):
t = t.replace("$tag",vobj.Object.Tag)
if hasattr(vobj.Object,"FinishFloor"):
t = t.replace("$floor",vobj.Object.FinishFloor)
if hasattr(vobj.Object,"FinishWalls"):
t = t.replace("$walls",vobj.Object.FinishWalls)
if hasattr(vobj.Object,"FinishCeiling"):
t = t.replace("$ceiling",vobj.Object.FinishCeiling)
if first:
text1.append(t.encode("utf8"))
else:
text2.append(t.encode("utf8"))
first = False
if text1:
self.text1.string.setValues(text1)
if text2:
self.text2.string.setValues(text2)
elif prop == "FontName":
if hasattr(self,"font") and hasattr(vobj,"FontName"):
self.font.name = str(vobj.FontName)
elif (prop == "FontSize"):
if hasattr(self,"font") and hasattr(vobj,"FontSize"):
self.font.size = vobj.FontSize.Value
elif (prop == "FirstLine"):
if hasattr(self,"header") and hasattr(vobj,"FontSize") and hasattr(vobj,"FirstLine"):
scale = vobj.FirstLine.Value/vobj.FontSize.Value
self.header.scaleFactor.setValue([scale,scale,scale])
elif prop == "TextColor":
if hasattr(self,"color") and hasattr(vobj,"TextColor"):
c = vobj.TextColor
self.color.rgb.setValue(c[0],c[1],c[2])
elif prop == "TextPosition":
if hasattr(self,"coords") and hasattr(self,"header") and hasattr(vobj,"TextPosition") and hasattr(vobj,"FirstLine"):
pos = self.getTextPosition(vobj)
self.coords.translation.setValue([pos.x,pos.y,pos.z])
up = vobj.FirstLine.Value * vobj.LineSpacing
self.header.translation.setValue([0,up,0])
elif prop == "LineSpacing":
if hasattr(self,"text1") and hasattr(self,"text2") and hasattr(vobj,"LineSpacing"):
self.text1.spacing = vobj.LineSpacing
self.text2.spacing = vobj.LineSpacing
self.onChanged(vobj,"TextPosition")
elif prop == "TextAlign":
if hasattr(self,"text1") and hasattr(self,"text2") and hasattr(vobj,"TextAlign"):
from pivy import coin
if vobj.TextAlign == "Center":
self.text1.justification = coin.SoAsciiText.CENTER
self.text2.justification = coin.SoAsciiText.CENTER
elif vobj.TextAlign == "Right":
self.text1.justification = coin.SoAsciiText.RIGHT
self.text2.justification = coin.SoAsciiText.RIGHT
else:
self.text1.justification = coin.SoAsciiText.LEFT
self.text2.justification = coin.SoAsciiText.LEFT
elif prop == "Visibility":
if vobj.Visibility:
self.label.whichChild = 0
else:
self.label.whichChild = -1
#* *
#***************************************************************************
import math
import FreeCAD as App
import FreeCADGui as Gui
from FreeCAD import Vector, Matrix, Placement
import Part
from FreeCAD import Units
import Instance as ShipInstance
import WeightInstance
import TankInstance
from shipHydrostatics import Tools as Hydrostatics
G = Units.parseQuantity("9.81 m/s^2")
MAX_EQUILIBRIUM_ITERS = 10
DENS = Units.parseQuantity("1025 kg/m^3")
TRIM_RELAX_FACTOR = 10.0
def solve(ship, weights, tanks, rolls, var_trim=True):
"""Compute the ship GZ stability curve
Position arguments:
ship -- Ship object
weights -- List of weights to consider
tanks -- List of tanks to consider (each one should be a tuple with the
tank instance, the density of the fluid inside, and the filling level ratio)
rolls -- List of roll angles
#* *
#***************************************************************************
import math
import random
from FreeCAD import Vector, Rotation, Matrix, Placement
import Part
from FreeCAD import Units
import FreeCAD as App
import FreeCADGui as Gui
from PySide import QtGui, QtCore
from .. import Instance
from ..shipUtils import Math
from ..shipUtils import Units as USys
DENS = Units.parseQuantity("1025 kg/m^3") # Salt water
COMMON_BOOLEAN_ITERATIONS = 10
def placeShipShape(shape, draft, roll, trim):
"""Move the ship shape such that the free surface matches with the plane
z=0. The transformation will be applied on the input shape, so copy it
before calling this method if it should be preserved.
Position arguments:
shape -- Ship shape
draft -- Ship draft
roll -- Roll angle
trim -- Trim angle
Returned values:
def get_distances(self):
"""Get the distance parameters from the widgets."""
r_d_str = self.form.spinbox_r_distance.text()
tan_d_str = self.form.spinbox_tan_distance.text()
return (U.Quantity(r_d_str).Value,
U.Quantity(tan_d_str).Value)
def process_output(self, text):
log_lines = text.split('\n')
prev_niter = self.niter
for line in log_lines:
line = line.rstrip()
split = line.split()
# Only record the first residual per outer iteration
if line.startswith(u"Time = "):
try:
time_val = float(line.lstrip(u"Time = "))
except ValueError:
pass
else:
self.prev_time = self.latest_time
self.latest_time = time_val
self.prev_num_outer_iters = self.latest_outer_iter
if self.latest_time > 0:
# Don't keep spurious time zero
self.latest_outer_iter = 0
self.niter += 1
self.in_forces_section = None
self.in_forcecoeffs_section = None
if line.find(u"PIMPLE: iteration ") >= 0 or line.find(
u"pseudoTime: iteration ") >= 0:
self.latest_outer_iter += 1
# Don't increment counter on first outer iter as this was already done with time
if self.latest_outer_iter > 1:
self.niter += 1
if line.startswith(u"forces") and (line.endswith(u"write:")
or line.endswith(u"execute:")):
self.in_forces_section = split[1]
if line.startswith(u"forceCoeffs") and (
line.endswith(u"write:") or line.endswith(u"execute:")):
self.in_forcecoeffs_section = split[1]
if not line.strip():
# Blank line
self.in_forces_section = None
self.in_forcecoeffs_section = None
# Add a point to the time axis for each outer iteration
if self.niter > len(self.time):
self.time.append(self.latest_time)
if self.latest_outer_iter > 0:
# Outer-iteration case
# Create virtual times to space the residuals of the outer iterations nicely on the time graph
self.prev_num_outer_iters = max(self.prev_num_outer_iters,
self.latest_outer_iter)
for i in range(self.latest_outer_iter):
self.time[-(
self.latest_outer_iter - i)] = self.prev_time + (
self.latest_time - self.prev_time) * (
(i + 1) / self.prev_num_outer_iters)
if "Ux," in split and self.niter > len(self.UxResiduals):
self.UxResiduals.append(float(split[7].split(',')[0]))
if "Uy," in split and self.niter > len(self.UyResiduals):
self.UyResiduals.append(float(split[7].split(',')[0]))
if "Uz," in split and self.niter > len(self.UzResiduals):
self.UzResiduals.append(float(split[7].split(',')[0]))
if "p," in split and self.niter > len(self.pResiduals):
self.pResiduals.append(float(split[7].split(',')[0]))
if "p_rgh," in split and self.niter > len(self.pResiduals):
self.pResiduals.append(float(split[7].split(',')[0]))
if "h," in split and self.niter > len(self.EResiduals):
self.EResiduals.append(float(split[7].split(',')[0]))
# HiSA coupled residuals
if "Residual:" in split and self.niter > len(self.rhoResiduals):
self.rhoResiduals.append(float(split[4]))
self.UxResiduals.append(float(split[5].lstrip('(')))
self.UyResiduals.append(float(split[6]))
self.UzResiduals.append(float(split[7].rstrip(')')))
self.EResiduals.append(float(split[8]))
if "k," in split and self.niter > len(self.kResiduals):
self.kResiduals.append(float(split[7].split(',')[0]))
if "epsilon," in split and self.niter > len(self.epsilonResiduals):
self.epsilonResiduals.append(float(split[7].split(',')[0]))
if "omega," in split and self.niter > len(self.omegaResiduals):
self.omegaResiduals.append(float(split[7].split(',')[0]))
if "nuTilda," in split and self.niter > len(self.nuTildaResiduals):
self.nuTildaResiduals.append(float(split[7].split(',')[0]))
if "gammaInt," in split and self.niter > len(
self.gammaIntResiduals):
self.gammaIntResiduals.append(float(split[7].split(',')[0]))
if "ReThetat," in split and self.niter > len(
self.ReThetatResiduals):
self.ReThetatResiduals.append(float(split[7].split(',')[0]))
# Force monitors
if self.in_forces_section:
f = self.forces[self.in_forces_section]
if (("Pressure" in split) or
("pressure"
in split)) and self.niter - 1 > len(f['pressureXForces']):
f['pressureXForces'].append(float(split[2].lstrip("(")))
f['pressureYForces'].append(float(split[3]))
f['pressureZForces'].append(float(split[4].rstrip(")")))
if (("Viscous" in split) or
("viscous"
in split)) and self.niter - 1 > len(f['viscousXForces']):
f['viscousXForces'].append(float(split[2].lstrip("(")))
f['viscousYForces'].append(float(split[3]))
f['viscousZForces'].append(float(split[4].rstrip(")")))
# Force coefficient monitors
if self.in_forcecoeffs_section:
fc = self.force_coeffs[self.in_forcecoeffs_section]
if "Cd" in split and self.niter - 1 > len(fc['cdCoeffs']):
fc['cdCoeffs'].append(float(split[2]))
if "Cl" in split and self.niter - 1 > len(fc['clCoeffs']):
fc['clCoeffs'].append(float(split[2]))
# Update plots
if self.niter > 1 and self.niter > prev_niter:
self.solver.Proxy.residual_plotter.updateValues(
self.time,
OrderedDict([('$\\rho$', self.rhoResiduals),
('$U_x$', self.UxResiduals),
('$U_y$', self.UyResiduals),
('$U_z$', self.UzResiduals),
('$p$', self.pResiduals),
('$E$', self.EResiduals),
('$k$', self.kResiduals),
('$\\epsilon$', self.epsilonResiduals),
('$\\tilde{\\nu}$', self.nuTildaResiduals),
('$\\omega$', self.omegaResiduals),
('$\\gamma$', self.gammaIntResiduals),
('$Re_{\\theta}$', self.ReThetatResiduals)]))
for fn in self.forces:
f = self.forces[fn]
self.solver.Proxy.forces_plotters[fn].updateValues(
self.time,
OrderedDict([('$Pressure_x$', f['pressureXForces']),
('$Pressure_y$', f['pressureYForces']),
('$Pressure_z$', f['pressureZForces']),
('$Viscous_x$', f['viscousXForces']),
('$Viscous_y$', f['viscousYForces']),
('$Viscous_z$', f['viscousZForces'])]))
for fcn in self.force_coeffs:
fc = self.force_coeffs[fcn]
self.solver.Proxy.force_coeffs_plotters[fcn].updateValues(
self.time,
OrderedDict([('$C_D$', fc['cdCoeffs']),
('$C_L$', fc['clCoeffs'])]))
# Probes
for pn in self.probes:
p = self.probes[pn]
if p['file'] is None:
working_dir = CfdTools.getOutputPath(self.analysis)
case_name = self.solver.InputCaseName
solver_dir = os.path.abspath(
os.path.join(working_dir, case_name))
try:
f = open(
os.path.join(solver_dir, 'postProcessing', pn, '0',
p['field']))
p['file'] = f
except OSError:
pass
if p['file']:
ntimes = len(p['time'])
is_vector = False
for l in p['file'].readlines():
l = l.strip()
if len(l) and not l.startswith('#'):
s = l.split()
p['time'].append(float(s[0]))
if s[1].startswith('('):
is_vector = True
while len(p['values']) < len(s) - 1:
p['values'].append([])
for i in range(1, len(s)):
s[i] = s[i].lstrip('(').rstrip(')')
p['values'][i - 1].append(float(s[i]))
if len(p['time']) > ntimes:
legends = []
for pi in p['points']:
points_str = '({}, {}, {}) m'.format(
*(Units.Quantity(pij, Units.Length).getValueAs('m')
for pij in (pi.x, pi.y, pi.z)))
if is_vector:
legends.append('{}$_x$ @ '.format(p['field']) +
points_str)
legends.append('{}$_y$ @ '.format(p['field']) +
points_str)
legends.append('{}$_z$ @ '.format(p['field']) +
points_str)
else:
legends.append('${}$ @ '.format(p['field']) +
points_str)
self.solver.Proxy.probes_plotters[pn].updateValues(
p['time'], OrderedDict(zip(legends, p['values'])))
#***************************************************************************
import math
import random
from FreeCAD import Vector, Rotation, Matrix, Placement
import Part
from FreeCAD import Units
import FreeCAD as App
import FreeCADGui as Gui
from PySide import QtGui, QtCore
import Instance
from shipUtils import Math
import shipUtils.Units as USys
DENS = Units.parseQuantity("1025 kg/m^3") # Salt water
COMMON_BOOLEAN_ITERATIONS = 10
def placeShipShape(shape, draft, roll, trim):
"""Move the ship shape such that the free surface matches with the plane
z=0. The transformation will be applied on the input shape, so copy it
before calling this method if it should be preserved.
Position arguments:
shape -- Ship shape
draft -- Ship draft
roll -- Roll angle
trim -- Trim angle
Returned values:
def get_region_data(self):
# mesh regions
self.ele_length_map = {} # { 'ElementString' : element length }
self.ele_node_map = {} # { 'ElementString' : [element nodes] }
if not self.mesh_obj.MeshRegionList:
print(' No mesh regions.')
else:
print(' Mesh regions, we need to get the elements.')
# by the use of MeshRegion object and a BooleanSplitCompound there could be problems with node numbers see
# http://forum.freecadweb.org/viewtopic.php?f=18&t=18780&start=40#p149467
# http://forum.freecadweb.org/viewtopic.php?f=18&t=18780&p=149520#p149520
part = self.part_obj
if self.mesh_obj.MeshRegionList:
if part.Shape.ShapeType == "Compound" and hasattr(
part, "Proxy"
): # other part obj might not have a Proxy, thus an exception would be raised
if (part.Proxy.Type == "FeatureBooleanFragments"
or part.Proxy.Type == "FeatureSlice"
or part.Proxy.Type == "FeatureXOR"):
error_message = " The mesh to shape is a boolean split tools Compound and the mesh has mesh region list. GMSH could return unexpected meshes in such circumstances. It is strongly recommended to extract the shape to mesh from the Compound and use this one."
FreeCAD.Console.PrintError(error_message + "\n")
# TODO no gui popup because FreeCAD will be in a endless prind loop as long as the pop up is on --> my be find a better solution for either of both --> thus the pop up is in task panel
for mr_obj in self.mesh_obj.MeshRegionList:
# print(mr_obj.Name)
# print(mr_obj.CharacteristicLength)
# print(Units.Quantity(mr_obj.CharacteristicLength).Value)
if mr_obj.CharacteristicLength:
if mr_obj.References:
for sub in mr_obj.References:
# print(sub[0]) # Part the elements belongs to
# check if the shape of the mesh region is an element of the Part to mesh, if not try to find the element in the shape to mesh
search_ele_in_shape_to_mesh = False
if not self.part_obj.Shape.isSame(sub[0].Shape):
# print(" One element of the meshregion " + mr_obj.Name + " is not an element of the Part to mesh.")
# print(" But we gone try to find it in the Shape to mesh :-)")
search_ele_in_shape_to_mesh = True
for elems in sub[1]:
# print(elems) # elems --> element
if search_ele_in_shape_to_mesh:
# we gone try to find the element it in the Shape to mesh and use the found element as elems
ele_shape = FemMeshTools.get_element(
sub[0], elems
) # the method getElement(element) does not return Solid elements
found_element = FemMeshTools.find_element_in_shape(
self.part_obj.Shape, ele_shape)
if found_element:
elems = found_element
else:
FreeCAD.Console.PrintError(
"One element of the meshregion " +
mr_obj.Name +
" could not be found in the Part to mesh. It will be ignored.\n"
)
# print(elems) # element
if elems not in self.ele_length_map:
self.ele_length_map[
elems] = Units.Quantity(
mr_obj.CharacteristicLength).Value
else:
FreeCAD.Console.PrintError(
"The element " + elems +
" of the meshregion " + mr_obj.Name +
" has been added to another mesh region.\n"
)
else:
FreeCAD.Console.PrintError(
"The meshregion: " + mr_obj.Name +
" is not used to create the mesh because the reference list is empty.\n"
)
else:
FreeCAD.Console.PrintError(
"The meshregion: " + mr_obj.Name +
" is not used to create the mesh because the CharacteristicLength is 0.0 mm.\n"
)
for eleml in self.ele_length_map:
ele_shape = FemMeshTools.get_element(
self.part_obj, eleml
) # the method getElement(element) does not return Solid elements
ele_vertexes = FemMeshTools.get_vertexes_by_element(
self.part_obj.Shape, ele_shape)
self.ele_node_map[eleml] = ele_vertexes
print(' {}'.format(self.ele_length_map))
print(' {}'.format(self.ele_node_map))
def displacement(ship, draft=None,
roll=Units.parseQuantity("0 deg"),
trim=Units.parseQuantity("0 deg")):
"""Compute the ship displacement
Position arguments:
ship -- Ship object (see createShip)
Keyword arguments:
draft -- Ship draft (Design ship draft by default)
roll -- Roll angle (0 degrees by default)
trim -- Trim angle (0 degrees by default)
Returned values:
disp -- The ship displacement (a density of the water of 1025 kg/m^3 is
assumed)
B -- Bouyance application point, i.e. Center of mass of the underwater side
Cb -- Block coefficient
The Bouyance center is referred to the original ship position.
"""
if draft is None:
draft = ship.Draft
shape, base_z = placeShipShape(ship.Shape.copy(), draft, roll, trim)
shape = getUnderwaterSide(shape)
vol = 0.0
cog = Vector()
if len(shape.Solids) > 0:
for solid in shape.Solids:
vol += solid.Volume
sCoG = solid.CenterOfMass
cog.x = cog.x + sCoG.x * solid.Volume
cog.y = cog.y + sCoG.y * solid.Volume
cog.z = cog.z + sCoG.z * solid.Volume
cog.x = cog.x / vol
cog.y = cog.y / vol
cog.z = cog.z / vol
bbox = shape.BoundBox
Vol = (bbox.XMax - bbox.XMin) * (bbox.YMax - bbox.YMin) * abs(bbox.ZMin)
# Undo the transformations on the bouyance point
B = Part.Point(Vector(cog.x, cog.y, cog.z))
m = Matrix()
m.move(Vector(0.0, 0.0, draft))
m.move(Vector(-draft * math.sin(trim.getValueAs("rad")), 0.0, 0.0))
m.rotateY(trim.getValueAs("rad"))
m.move(Vector(0.0,
-draft * math.sin(roll.getValueAs("rad")),
base_z))
m.rotateX(-roll.getValueAs("rad"))
B.transform(m)
try:
cb = vol / Vol
except ZeroDivisionError:
msg = QtGui.QApplication.translate(
"ship_console",
"ZeroDivisionError: Null volume found during the displacement"
" computation!",
None)
App.Console.PrintError(msg + '\n')
cb = 0.0
# Return the computed data
return (DENS * Units.Quantity(vol, Units.Volume),
Vector(B.X, B.Y, B.Z),
cb)
def parse(pathobj):
global DRILL_RETRACT_MODE
global MOTION_MODE
global CURRENT_X
global CURRENT_Y
global CURRENT_Z
out = ""
lastcommand = None
precision_string = '.' + str(PRECISION) + 'f'
params = [
'X', 'Y', 'Z', 'A', 'B', 'C', 'U', 'V', 'W', 'I', 'J', 'K', 'F', 'S',
'T', 'Q', 'R', 'L', 'P'
]
if hasattr(pathobj, "Group"): # We have a compound or project.
if OUTPUT_COMMENTS:
out += linenumber() + "(Compound: " + pathobj.Label + ")\n"
for p in pathobj.Group:
out += parse(p)
return out
else: # parsing simple path
if not hasattr(
pathobj,
"Path"): # groups might contain non-path things like stock.
return out
if OUTPUT_COMMENTS:
out += linenumber() + "(Path: " + pathobj.Label + ")\n"
for c in pathobj.Path.Commands:
outstring = []
command = c.Name
outstring.append(command)
# if modal: only print the command if it is not the same as the last one
if MODAL:
if command == lastcommand:
outstring.pop(0)
# Now add the remaining parameters in order
for param in params:
if param in c.Parameters:
if param == 'F':
if command not in RAPID_MOVES:
speed = Units.Quantity(c.Parameters['F'],
FreeCAD.Units.Velocity)
if speed.getValueAs(UNIT_SPEED_FORMAT) > 0.0:
outstring.append(param + format(
float(speed.getValueAs(UNIT_SPEED_FORMAT)),
precision_string))
elif param in ['T', 'H', 'D', 'S', 'P', 'L']:
outstring.append(param + str(c.Parameters[param]))
elif param in ['A', 'B', 'C']:
outstring.append(
param +
format(c.Parameters[param], precision_string))
else: # [X, Y, Z, U, V, W, I, J, K, R, Q] (Conversion eventuelle mm/inches)
pos = Units.Quantity(c.Parameters[param],
FreeCAD.Units.Length)
outstring.append(
param + format(float(pos.getValueAs(UNIT_FORMAT)),
precision_string))
# store the latest command
lastcommand = command
# Memorizes the current position for calculating the related movements and the withdrawal plan
if command in MOTION_COMMANDS:
if 'X' in c.Parameters:
CURRENT_X = Units.Quantity(c.Parameters['X'],
FreeCAD.Units.Length)
if 'Y' in c.Parameters:
CURRENT_Y = Units.Quantity(c.Parameters['Y'],
FreeCAD.Units.Length)
if 'Z' in c.Parameters:
CURRENT_Z = Units.Quantity(c.Parameters['Z'],
FreeCAD.Units.Length)
if command in ('G98', 'G99'):
DRILL_RETRACT_MODE = command
if command in ('G90', 'G91'):
MOTION_MODE = command
if TRANSLATE_DRILL_CYCLES:
if command in ('G81', 'G82', 'G83'):
out += drill_translate(outstring, command, c.Parameters)
# Erase the line we just translated
outstring = []
if SPINDLE_WAIT > 0:
if command in ('M3', 'M03', 'M4', 'M04'):
out += linenumber() + format_outstring(outstring) + "\n"
out += linenumber() + format_outstring(
['G4', 'P%s' % SPINDLE_WAIT]) + "\n"
outstring = []
# Check for Tool Change:
if command in ('M6', 'M06'):
if OUTPUT_COMMENTS:
out += linenumber() + "(Begin toolchange)\n"
if not OUTPUT_TOOL_CHANGE:
outstring.insert(0, "(")
outstring.append(")")
else:
for line in TOOL_CHANGE.splitlines(True):
out += linenumber() + line
if command == "message":
if OUTPUT_COMMENTS is False:
out = []
else:
outstring.pop(0) # remove the command
if command in SUPPRESS_COMMANDS:
outstring.insert(0, "(")
outstring.append(")")
# prepend a line number and append a newline
if len(outstring) >= 1:
out += linenumber() + format_outstring(outstring) + "\n"
return out
def processRefinements(self):
""" Process mesh refinements """
mr_objs = CfdTools.getMeshRefinementObjs(self.mesh_obj)
if self.mesh_obj.MeshUtility == "gmsh":
# mesh regions
self.ele_length_map = {} # { 'ElementString' : element length }
self.ele_node_map = {} # { 'ElementString' : [element nodes] }
if not mr_objs:
print(' No mesh refinements')
else:
print(' Mesh refinements found - getting elements')
if self.part_obj.Shape.ShapeType == 'Compound':
# see http://forum.freecadweb.org/viewtopic.php?f=18&t=18780&start=40#p149467 and http://forum.freecadweb.org/viewtopic.php?f=18&t=18780&p=149520#p149520
err = "GMSH could return unexpected meshes for a boolean split tools Compound. It is strongly recommended to extract the shape to mesh from the Compound and use this one."
FreeCAD.Console.PrintError(err + "\n")
for mr_obj in mr_objs:
if mr_obj.RelativeLength:
if mr_obj.References:
for sub in mr_obj.References:
# Check if the shape of the mesh region is an element of the Part to mesh;
# if not try to find the element in the shape to mesh
search_ele_in_shape_to_mesh = False
ref = FreeCAD.ActiveDocument.getObject(sub[0])
if not self.part_obj.Shape.isSame(ref.Shape):
search_ele_in_shape_to_mesh = True
elems = sub[1]
if search_ele_in_shape_to_mesh:
# Try to find the element in the Shape to mesh
ele_shape = FemMeshTools.get_element(
ref, elems
) # the method getElement(element) does not return Solid elements
found_element = CfdTools.findElementInShape(
self.part_obj.Shape, ele_shape)
if found_element:
elems = found_element
else:
FreeCAD.Console.PrintError(
"One element of the meshregion " +
mr_obj.Name +
" could not be found in the Part to mesh. It will be ignored.\n"
)
elems = None
if elems:
if elems not in self.ele_length_map:
# self.ele_length_map[elems] = Units.Quantity(mr_obj.CharacteristicLength).Value
mr_rellen = mr_obj.RelativeLength
if mr_rellen > 1.0:
mr_rellen = 1.0
FreeCAD.Console.PrintError(
"The meshregion: " +
mr_obj.Name +
" should not use a relative length greater than unity.\n"
)
elif mr_rellen < 0.01:
mr_rellen = 0.01 # Relative length should not be less than 1/100 of base length
FreeCAD.Console.PrintError(
"The meshregion: " +
mr_obj.Name +
" should not use a relative length smaller than 0.01.\n"
)
self.ele_length_map[
elems] = mr_rellen * self.clmax
else:
FreeCAD.Console.PrintError(
"The element " + elems +
" of the mesh refinement " +
mr_obj.Name +
" has been added to another mesh refinement.\n"
)
else:
FreeCAD.Console.PrintError(
"The meshregion: " + mr_obj.Name +
" is not used to create the mesh because the reference list is empty.\n"
)
else:
FreeCAD.Console.PrintError(
"The meshregion: " + mr_obj.Name +
" is not used to create the mesh because the CharacteristicLength is 0.0 mm.\n"
)
for eleml in self.ele_length_map:
ele_shape = FemMeshTools.get_element(
self.part_obj, eleml
) # the method getElement(element) does not return Solid elements
ele_vertexes = FemMeshTools.get_vertexes_by_element(
self.part_obj.Shape, ele_shape)
self.ele_node_map[eleml] = ele_vertexes
else:
cf_settings = self.cf_settings
cf_settings['MeshRegions'] = {}
cf_settings['BoundaryLayers'] = {}
cf_settings['InternalRegions'] = {}
snappy_settings = self.snappy_settings
snappy_settings['MeshRegions'] = {}
snappy_settings['InternalRegions'] = {}
from collections import defaultdict
ele_meshpatch_map = defaultdict(list)
if not mr_objs:
print(' No mesh refinement')
else:
print(' Mesh refinements - getting the elements')
if "Boolean" in self.part_obj.Name:
err = "Cartesian meshes should not be generated for boolean split compounds."
FreeCAD.Console.PrintError(err + "\n")
# Make list of list of all references for their corresponding mesh object
bl_matched_faces = []
if self.mesh_obj.MeshUtility == 'cfMesh':
region_face_lists = []
for mr_id, mr_obj in enumerate(mr_objs):
region_face_lists.append([])
if mr_obj.NumberLayers > 1 and not mr_obj.Internal:
refs = mr_obj.References
for r in refs:
region_face_lists[mr_id].append(r)
CfdTools.cfdMessage("Matching refinement regions")
bl_matched_faces = CfdTools.matchFacesToTargetShape(
region_face_lists, self.mesh_obj.Part.Shape)
for mr_id, mr_obj in enumerate(mr_objs):
Internal = mr_obj.Internal
if mr_obj.RelativeLength:
# Store parameters per region
mr_rellen = mr_obj.RelativeLength
if mr_rellen > 1.0:
mr_rellen = 1.0
FreeCAD.Console.PrintError(
"The meshregion: {} should not use a relative length greater "
"than unity.\n".format(mr_obj.Name))
elif mr_rellen < 0.001:
mr_rellen = 0.001 # Relative length should not be less than 0.1% of base length
FreeCAD.Console.PrintError(
"The meshregion: {} should not use a relative length smaller "
"than 0.001.\n".format(mr_obj.Name))
if not (self.mesh_obj.MeshUtility == 'snappyHexMesh'
and mr_obj.Baffle):
fid = open(
os.path.join(self.triSurfaceDir,
mr_obj.Name + '.stl'), 'w')
snappy_mesh_region_list = []
patch_list = []
for (si, sub) in enumerate(mr_obj.References):
shape = FreeCAD.ActiveDocument.getObject(
sub[0]).Shape
elem = sub[1]
if self.mesh_obj.MeshUtility == 'snappyHexMesh' and mr_obj.Baffle:
# Save baffle references or faces individually
baffle = "{}{}{}".format(
mr_obj.Name, sub[0], elem)
fid = open(
os.path.join(self.triSurfaceDir,
baffle + ".stl"), 'w')
snappy_mesh_region_list.append(baffle)
if elem.startswith(
'Solid'
): # getElement doesn't work with solids for some reason
elt = shape.Solids[int(elem.lstrip('Solid')) -
1]
else:
elt = shape.getElement(elem)
if elt.ShapeType == 'Face' or elt.ShapeType == 'Solid':
CfdTools.cfdMessage(
"Triangulating part: {}:{} ...".format(
FreeCAD.ActiveDocument.getObject(
sub[0]).Label, sub[1]))
facemesh = MeshPart.meshFromShape(
elt,
LinearDeflection=self.mesh_obj.
STLLinearDeflection)
CfdTools.cfdMessage(" writing to file\n")
fid.write("solid {}{}{}\n".format(
mr_obj.Name, sub[0], elem))
for face in facemesh.Facets:
fid.write(" facet normal 0 0 0\n")
fid.write(" outer loop\n")
for i in range(3):
p = [
i * self.scale
for i in face.Points[i]
]
fid.write(
" vertex {} {} {}\n".format(
p[0], p[1], p[2]))
fid.write(" endloop\n")
fid.write(" endfacet\n")
fid.write("endsolid {}{}{}\n".format(
mr_obj.Name, sub[0], elem))
if self.mesh_obj.MeshUtility == 'snappyHexMesh' and mr_obj.Baffle:
fid.close()
if not (self.mesh_obj.MeshUtility == 'snappyHexMesh'
and mr_obj.Baffle):
fid.close()
if self.mesh_obj.MeshUtility == 'cfMesh' and mr_obj.NumberLayers > 1 and not Internal:
for (i, mf) in enumerate(bl_matched_faces):
for j in range(len(mf)):
if mr_id == mf[j][0]:
sfN = self.mesh_obj.ShapeFaceNames[i]
ele_meshpatch_map[mr_obj.Name].append(
sfN)
patch_list.append(sfN)
# Limit expansion ratio to greater than 1.0 and less than 1.2
expratio = mr_obj.ExpansionRatio
expratio = min(1.2, max(1.0, expratio))
cf_settings['BoundaryLayers'][
self.mesh_obj.
ShapeFaceNames[i]] = {
'NumberLayers':
mr_obj.NumberLayers,
'ExpansionRatio':
expratio,
'FirstLayerHeight':
self.scale * Units.Quantity(
mr_obj.FirstLayerHeight).
Value
}
if self.mesh_obj.MeshUtility == 'cfMesh':
if not Internal:
cf_settings['MeshRegions'][mr_obj.Name] = {
'RelativeLength':
mr_rellen * self.clmax * self.scale,
'RefinementThickness':
self.scale * Units.Quantity(
mr_obj.RefinementThickness).Value,
}
else:
cf_settings['InternalRegions'][mr_obj.Name] = {
'RelativeLength':
mr_rellen * self.clmax * self.scale
}
elif self.mesh_obj.MeshUtility == 'snappyHexMesh':
refinement_level = CfdTools.relLenToRefinementLevel(
mr_obj.RelativeLength)
if not Internal:
if not mr_obj.Baffle:
snappy_mesh_region_list.append(mr_obj.Name)
edge_level = CfdTools.relLenToRefinementLevel(
mr_obj.RegionEdgeRefinement)
for rL in range(len(snappy_mesh_region_list)):
mrName = mr_obj.Name + snappy_mesh_region_list[
rL]
snappy_settings['MeshRegions'][mrName] = {
'RegionName':
snappy_mesh_region_list[rL],
'RefinementLevel':
refinement_level,
'EdgeRefinementLevel':
edge_level,
'MaxRefinementLevel':
max(refinement_level, edge_level),
'Baffle':
mr_obj.Baffle
}
else:
snappy_settings['InternalRegions'][
mr_obj.Name] = {
'RefinementLevel': refinement_level
}
else:
FreeCAD.Console.PrintError(
"The meshregion: " + mr_obj.Name +
" is not used to create the mesh because the "
"CharacteristicLength is 0.0 mm or the reference list is empty.\n"
)
def drill_translate(outstring, cmd, params):
global DRILL_RETRACT_MODE
global MOTION_MODE
global CURRENT_X
global CURRENT_Y
global CURRENT_Z
global UNITS
global UNIT_FORMAT
global UNIT_SPEED_FORMAT
strFormat = '.' + str(PRECISION) + 'f'
trBuff = ""
if OUTPUT_COMMENTS: # Comment the original command
outstring[0] = "(" + outstring[0]
outstring[-1] = outstring[-1] + ")"
trBuff += linenumber() + format_outstring(outstring) + "\n"
# cycle conversion
# currently only cycles in XY are provided (G17)
# other plains ZX (G18) and YZ (G19) are not dealt with : Z drilling only.
drill_X = Units.Quantity(params['X'], FreeCAD.Units.Length)
drill_Y = Units.Quantity(params['Y'], FreeCAD.Units.Length)
drill_Z = Units.Quantity(params['Z'], FreeCAD.Units.Length)
RETRACT_Z = Units.Quantity(params['R'], FreeCAD.Units.Length)
# R less than Z is error
if RETRACT_Z < drill_Z:
trBuff += linenumber() + "(drill cycle error: R less than Z )\n"
return trBuff
if MOTION_MODE == 'G91': # G91 relative movements
drill_X += CURRENT_X
drill_Y += CURRENT_Y
drill_Z += CURRENT_Z
RETRACT_Z += CURRENT_Z
if DRILL_RETRACT_MODE == 'G98' and CURRENT_Z >= RETRACT_Z:
RETRACT_Z = CURRENT_Z
# get the other parameters
drill_Speed = Units.Quantity(params['F'], FreeCAD.Units.Velocity)
if cmd == 'G83':
drill_Step = Units.Quantity(params['Q'], FreeCAD.Units.Length)
a_bit = drill_Step * 0.05 # NIST 3.5.16.4 G83 Cycle: "current hole bottom, backed off a bit."
elif cmd == 'G82':
drill_DwellTime = params['P']
# wrap this block to ensure machine MOTION_MODE is restored in case of error
try:
if MOTION_MODE == 'G91':
trBuff += linenumber(
) + "G90\n" # force absolute coordinates during cycles
strG0_RETRACT_Z = 'G0 Z' + format(
float(RETRACT_Z.getValueAs(UNIT_FORMAT)), strFormat) + "\n"
strF_Drill_Speed = ' F' + format(
float(drill_Speed.getValueAs(UNIT_SPEED_FORMAT)), '.2f') + "\n"
# preliminary mouvement(s)
if CURRENT_Z < RETRACT_Z:
trBuff += linenumber() + strG0_RETRACT_Z
trBuff += linenumber() + 'G0 X' + format(
float(drill_X.getValueAs(UNIT_FORMAT)), strFormat) + ' Y' + format(
float(drill_Y.getValueAs(UNIT_FORMAT)), strFormat) + "\n"
if CURRENT_Z > RETRACT_Z:
# trBuff += linenumber() + 'G0 Z' + format(float(CURRENT_Z.getValueAs(UNIT_FORMAT)), strFormat) + "\n" # not following NIST 3.5.16.1 Preliminary and In-Between Motion
trBuff += linenumber() + strG0_RETRACT_Z
last_Stop_Z = RETRACT_Z
# drill moves
if cmd in ('G81', 'G82'):
trBuff += linenumber() + 'G1 Z' + format(
float(drill_Z.getValueAs(UNIT_FORMAT)),
strFormat) + strF_Drill_Speed
# pause where applicable
if cmd == 'G82':
trBuff += linenumber() + 'G4 P' + str(drill_DwellTime) + "\n"
trBuff += linenumber() + strG0_RETRACT_Z
else: # 'G83'
if params['Q'] != 0:
while 1:
if last_Stop_Z != RETRACT_Z:
clearance_depth = last_Stop_Z + a_bit
trBuff += linenumber() + 'G0 Z' + format(
float(clearance_depth.getValueAs(UNIT_FORMAT)),
strFormat) + "\n"
next_Stop_Z = last_Stop_Z - drill_Step
if next_Stop_Z > drill_Z:
trBuff += linenumber() + 'G1 Z' + format(
float(next_Stop_Z.getValueAs(UNIT_FORMAT)),
strFormat) + strF_Drill_Speed
trBuff += linenumber() + strG0_RETRACT_Z
last_Stop_Z = next_Stop_Z
else:
trBuff += linenumber() + 'G1 Z' + format(
float(drill_Z.getValueAs(UNIT_FORMAT)),
strFormat) + strF_Drill_Speed
trBuff += linenumber() + strG0_RETRACT_Z
break
except Exception as e:
pass
if MOTION_MODE == 'G91':
trBuff += linenumber() + 'G91' # Restore if changed
return trBuff
def areas(ship,
n,
draft=None,
roll=Units.parseQuantity("0 deg"),
trim=Units.parseQuantity("0 deg")):
"""Compute the ship transversal areas
Position arguments:
ship -- Ship object (see createShip)
n -- Number of points to compute
Keyword arguments:
draft -- Ship draft (Design ship draft by default)
roll -- Roll angle (0 degrees by default)
trim -- Trim angle (0 degrees by default)
Returned value:
List of sections, each section contains 2 values, the x longitudinal
coordinate, and the transversal area. If n < 2, an empty list will be
returned.
"""
if n < 2:
return []
if draft is None:
draft = ship.Draft
shape, _ = placeShipShape(ship.Shape.copy(), draft, roll, trim)
shape = getUnderwaterSide(shape)
# Sections distance computation
bbox = shape.BoundBox
xmin = bbox.XMin
xmax = bbox.XMax
dx = (xmax - xmin) / (n - 1.0)
# Since we are computing the sections in the total length (not in the
# length between perpendiculars), we can grant that the starting and
# ending sections have null area
areas = [(Units.Quantity(xmin,
Units.Length), Units.Quantity(0.0, Units.Area))]
# And since we just need to compute areas we will create boxes with its
# front face at the desired transversal area position, computing the
# common solid part, dividing it by faces, and getting only the desired
# ones.
App.Console.PrintMessage("Computing transversal areas...\n")
App.Console.PrintMessage("Some Inventor representation errors can be"
" shown, please ignore them.\n")
for i in range(1, n - 1):
App.Console.PrintMessage("{0} / {1}\n".format(i, n - 2))
x = xmin + i * dx
try:
f = Part.Face(shape.slice(Vector(1, 0, 0), x))
except Part.OCCError:
msg = QtGui.QApplication.translate(
"ship_console",
"Part.OCCError: Transversal area computation failed", None)
App.Console.PrintError(msg + '\n')
areas.append((Units.Quantity(x, Units.Length),
Units.Quantity(0.0, Units.Area)))
continue
# It is a valid face, so we can add this area
areas.append(
(Units.Quantity(x,
Units.Length), Units.Quantity(f.Area, Units.Area)))
# Last area is equal to zero (due to the total length usage)
areas.append(
(Units.Quantity(xmax, Units.Length), Units.Quantity(0.0, Units.Area)))
App.Console.PrintMessage("Done!\n")
return areas
def getClmax(self):
return Units.Quantity(self.clmax, Units.Length)
def displacement(ship,
draft=None,
roll=Units.parseQuantity("0 deg"),
trim=Units.parseQuantity("0 deg")):
"""Compute the ship displacement
Position arguments:
ship -- Ship object (see createShip)
Keyword arguments:
draft -- Ship draft (Design ship draft by default)
roll -- Roll angle (0 degrees by default)
trim -- Trim angle (0 degrees by default)
Returned values:
disp -- The ship displacement (a density of the water of 1025 kg/m^3 is
assumed)
B -- Bouyance application point, i.e. Center of mass of the underwater side
Cb -- Block coefficient
The Bouyance center is referred to the original ship position.
"""
if draft is None:
draft = ship.Draft
shape, base_z = placeShipShape(ship.Shape.copy(), draft, roll, trim)
shape = getUnderwaterSide(shape)
vol = 0.0
cog = Vector()
if len(shape.Solids) > 0:
for solid in shape.Solids:
vol += solid.Volume
sCoG = solid.CenterOfMass
cog.x = cog.x + sCoG.x * solid.Volume
cog.y = cog.y + sCoG.y * solid.Volume
cog.z = cog.z + sCoG.z * solid.Volume
cog.x = cog.x / vol
cog.y = cog.y / vol
cog.z = cog.z / vol
bbox = shape.BoundBox
Vol = (bbox.XMax - bbox.XMin) * (bbox.YMax - bbox.YMin) * abs(bbox.ZMin)
# Undo the transformations on the bouyance point
B = Part.Point(Vector(cog.x, cog.y, cog.z))
m = Matrix()
m.move(Vector(0.0, 0.0, draft))
m.move(Vector(-draft * math.sin(trim.getValueAs("rad")), 0.0, 0.0))
m.rotateY(trim.getValueAs("rad"))
m.move(Vector(0.0, -draft * math.sin(roll.getValueAs("rad")), base_z))
m.rotateX(-roll.getValueAs("rad"))
B.transform(m)
try:
cb = vol / Vol
except ZeroDivisionError:
msg = QtGui.QApplication.translate(
"ship_console",
"ZeroDivisionError: Null volume found during the displacement"
" computation!", None)
App.Console.PrintError(msg + '\n')
cb = 0.0
# Return the computed data
return (DENS * Units.Quantity(vol, Units.Volume), Vector(B.X, B.Y,
B.Z), cb)
def accept(self):
if not self.ship:
return False
if self.running:
return
self.save()
mw = self.getMainWindow()
form = mw.findChild(QtGui.QWidget, "TaskPanel")
form.trim = self.widget(QtGui.QLineEdit, "Trim")
form.minDraft = self.widget(QtGui.QLineEdit, "MinDraft")
form.maxDraft = self.widget(QtGui.QLineEdit, "MaxDraft")
form.nDraft = self.widget(QtGui.QSpinBox, "NDraft")
trim = Units.parseQuantity(Locale.fromString(form.trim.text()))
min_draft = Units.parseQuantity(Locale.fromString(form.minDraft.text()))
max_draft = Units.parseQuantity(Locale.fromString(form.maxDraft.text()))
n_draft = form.nDraft.value()
draft = min_draft
drafts = [draft]
dDraft = (max_draft - min_draft) / (n_draft - 1)
for i in range(1, n_draft):
draft = draft + dDraft
drafts.append(draft)
# Get external faces
self.loop = QtCore.QEventLoop()
self.timer = QtCore.QTimer()
self.timer.setSingleShot(True)
QtCore.QObject.connect(self.timer,
QtCore.SIGNAL("timeout()"),
self.loop,
QtCore.SLOT("quit()"))
self.running = True
faces = self.externalFaces(self.ship.Shape)
if not self.running:
return False
if len(faces) == 0:
msg = QtGui.QApplication.translate(
"ship_console",
"Failure detecting external faces from the ship object",
None)
App.Console.PrintError(msg + '\n')
return False
faces = Part.makeShell(faces)
# Get the hydrostatics
msg = QtGui.QApplication.translate(
"ship_console",
"Computing hydrostatics",
None)
App.Console.PrintMessage(msg + '...\n')
points = []
for i in range(len(drafts)):
App.Console.PrintMessage("\t{} / {}\n".format(i + 1, len(drafts)))
draft = drafts[i]
point = Tools.Point(self.ship,
faces,
draft,
trim)
points.append(point)
self.timer.start(0.0)
self.loop.exec_()
if(not self.running):
break
PlotAux.Plot(self.ship, trim, points)
return True