def _child_cells(self):
"""get all the child cells within the current cell,
defined by the miniribs
"""
cells = []
for leftrib, rightrib in\
itertools.izip(self.rib_profiles_3d[:-1], self.rib_profiles_3d[1:]):
cells.append(BasicCell(leftrib, rightrib))
if not self._miniribs:
return cells
ballooning = [self.rib1.ballooning[x] + self.rib2.ballooning[x] for x in self.x_values]
#for i in range(len(first.data)):
for index, (bl, left_point, right_point) in enumerate(itertools.izip(
ballooning, self._ribs[0].profile_3d.data, self._ribs[1].profile_3d.data
)):
l = norm(right_point - left_point) # L
lnew = sum([norm(c.prof1.data[index] - c.prof2.data[index]) for c in cells]) # L-NEW
for c in self._child_cells:
newval = lnew / l / bl
if newval < 1.:
c.ballooning_phi.append(arsinc(newval)) # B/L NEW 1 / (bl * l / lnew)
else:
c.ballooning_phi.append(arsinc(1.))
#raise ValueError("mull")
return cells
def _child_cells(self):
"""
get all the sub-cells within the current cell,
(separated by miniribs)
"""
cells = []
for leftrib, rightrib in zip(self.rib_profiles_3d[:-1],
self.rib_profiles_3d[1:]):
cells.append(BasicCell(leftrib, rightrib, ballooning=[]))
if not self.miniribs:
return cells
for index, xvalue in enumerate(self.x_values):
left_point = self.rib1.profile_3d.data[index]
right_point = self.rib2.profile_3d.data[index]
bl = self.ballooning[xvalue]
l = norm(right_point - left_point) # L
lnew = sum([
norm(c.prof1.data[index] - c.prof2.data[index]) for c in cells
]) # L-NEW
for c in cells:
if bl > 0:
newval = l / lnew * (bl + 1 / 2) - 1 / 2
#newval = l/lnew / bl
#newval = lnew / l / bl if bl != 0 else 1
c.ballooning_phi.append(
Ballooning.arcsinc(
1 / (1 + newval))) # B/L NEW 1 / (bl * l / lnew)
else:
c.ballooning_phi.append(0.)
return cells
def polygon_size(self):
size_min = float("inf")
size_max = float("-inf")
count = 0
sum = 0
for poly in self.all_polygons:
if len(poly) in (3, 4):
sides = []
for i in range(len(poly)):
i_plus = i + 1
if i_plus == len(poly):
i_plus = 0
side = np.array(list(poly[i])) - np.array(
list(poly[i_plus]))
sides.append(side)
if len(poly) == 3:
size_poly = 0.5 * vector.norm(np.cross(sides[0], sides[1]))
elif len(poly) == 4:
size_poly = 0.5 * (
vector.norm(np.cross(sides[0], sides[1])) +
vector.norm(np.cross(sides[2], sides[3])))
else:
size_poly = 0
sum += size_poly
count += 1
size_min = min(size_min, size_poly)
size_max = max(size_max, size_poly)
return size_min, size_max, sum / count
def area(self):
p1_1 = self.rib1.align([0, 0, 0])
p1_2 = self.rib1.align([1, 0, 0])
p2_1 = self.rib2.align([0, 0, 0])
p2_2 = self.rib2.align([1, 0, 0])
return 0.5 * (norm(np.cross(p1_2 - p1_1, p2_1 - p1_1)) +
norm(np.cross(p2_2 - p2_1, p2_2 - p1_2)))
def recalc(self):
if not self.rib2.profile_2d.numpoints == self.rib1.profile_2d.numpoints:
raise ValueError("Unequal length of Cell-Profiles")
xvalues = self.rib1.profile_2d.x_values
BasicCell.recalc(self)
self.prof1 = self.rib1.profile_3d
self.prof2 = self.rib2.profile_3d
#Map Ballooning
if not self.miniribs: # In case there is no midrib, The Cell represents itself!
self._cells = [self] # The cell itself is its cell, clear?
self._yvalues = [0, 1]
else:
self._cells = []
self._yvalues = [0] + [rib.y_value for rib in self.miniribs] + [1]
ballooning = [self.rib1.ballooning[x] + self.rib2.ballooning[x] for x in xvalues]
miniribs = sorted(self.miniribs, key=lambda rib: rib.y_value) # sort for cell-wide (y) argument.
first = self.rib1.profile_3d
for minirib in miniribs:
big = self.midrib_basic_cell(minirib.y_value, True).data
small = self.midrib_basic_cell(minirib.y_value, False).data
points = []
for i in range(len(big)): # Calculate Rib
fakt = minirib.function(xvalues[i]) # factor ballooned/unb. (0-1)
point = small[i] + fakt * (big[i] - small[i])
points.append(point)
minirib.data = points
second = minirib
self._cells.append(BasicCell(first, second, [])) # leave ballooning empty
first = second
#Last Sub-Cell
self._cells.append(BasicCell(first, self.rib2.profile_3d, []))
# Calculate ballooning for each x-value
# Hamilton Principle:
# http://en.wikipedia.org/wiki/Hamilton%27s_principle
# http://en.wikipedia.org/wiki/Hamilton%E2%80%93Jacobi_equation
# b' = b
# f' = f*(l/l') [f=b/l]
for i in range(len(first.data)):
bl = ballooning[i] + 1 # b/l -> *l/lnew
l = norm(self.rib2.profile_3d.data[i] - self.rib1.profile_3d.data[i]) # L
lnew = sum([norm(c.prof1.data[i] - c.prof2.data[i]) for c in self._cells]) # L-NEW
for c in self._cells:
newval = lnew / l / bl
if newval < 1.:
c.ballooning_phi.append(arsinc(newval)) # B/L NEW 1 / (bl * l / lnew)
else:
c.ballooning_phi.append(arsinc(1.))
#raise ValueError("mull")
for cell in self._cells:
cell.recalc()
def _mindist(self, newpoint):
np = array(newpoint)
pts = array([[pt.x, pt.y] for pt in self.ml.Object.points])
mindist0 = norm(pts[0] - np)
print(mindist0)
out = 0
count = 0
for pt in pts[1:]:
count += 1
mindist = norm(pt - np)
if mindist < mindist0:
out = count
return out
def _mindist(self, newpoint):
np = array(newpoint)
pts = array([[pt.x, pt.y] for pt in self.ml.Object.points])
mindist0 = norm(pts[0] - np)
print(mindist0)
out = 0
count = 0
for pt in pts[1:]:
count += 1
mindist = norm(pt - np)
if mindist < mindist0:
out = count
return out
def area(self):
area = 0.
if len(self.ribs) == 0:
return 0
front = self.get_spanwise(0)
back = self.get_spanwise(1)
front[0][1] = 0 # Get only half a midrib, if there is...
back[0][1] = 0
for i in range(len(front) - 1):
area += norm(numpy.cross(front[i] - front[i + 1], back[i + 1] - front[i + 1]))
area += norm(numpy.cross(back[i] - back[i + 1], back[i] - front[i]))
# By this we get twice the area of half the glider :)
# http://en.wikipedia.org/wiki/Triangle#Using_vectors
return area
def make_smooth_dist(self, points, num=70, dist=None, upper=True):
# make array [[lenght, x, y], ...]
if not dist:
return points
length = [0]
for i, point in enumerate(points[1:]):
length.append(length[-1] + norm(point - points[i]))
interpolation_x = Interpolation(zip(length, [p[0] for p in points]))
interpolation_y = Interpolation(points)
def get_point(dist):
x = interpolation_x(dist)
return [x, interpolation_y(x)]
if dist == "const":
dist = np.linspace(0, length[-1], num)
elif dist == "sin":
if upper:
dist = [
np.sin(i) * length[-1]
for i in np.linspace(0, np.pi / 2, num)
]
else:
dist = [
abs(1 - np.sin(i)) * length[-1]
for i in np.linspace(0, np.pi / 2, num)
]
else:
return points
return [get_point(d) for d in dist]
def midrib_basic_cell(self, y, ballooning=True, arc_argument=True):
if y == 0: # left side
return self.prof1
elif y == 1: # right side
return self.prof2
else: # somewhere
#self._checkxvals()
midrib = []
for i in range(len(self.prof1.data)): # Arc -> phi(bal) -> r # oder so...
diff = self.prof1[i] - self.prof2[i]
if ballooning and self.ballooning_radius[i] > 0.:
if arc_argument:
d = 0.5 - math.sin(self.ballooning_phi[i] * (0.5 - y)) / math.sin(self.ballooning_phi[i])
h = math.cos(self.ballooning_phi[i] * (1 - 2 * y)) - self.ballooning_cos_phi[i]
#h = math.sqrt(1 - (norm(diff) * (0.5 - d) / self._radius[i]) ** 2)
#h -= self._cosphi[i] # cosphi2-cosphi
else:
d = y
h = math.sqrt(1 - (norm(diff) * (0.5 - y) / self.ballooning_radius[i]) ** 2)
h -= self.ballooning_cos_phi[i] # cosphi2-cosphi
else: # Without ballooning
d = y
h = 0.
midrib.append(self.prof1[i] - diff * d + self.normvectors[i] * h * self.ballooning_radius[i])
return Profile3D(midrib)
def test_flat(self):
prof = self.rib.profile_2d.copy()
prof = PolyLine2D(prof.data) * [self.rib.chord, self.rib.chord]
print(self.rib.profile_2d, prof)
#prof.scale(self.rib.chord)
gib_pos = [n.rib_pos for n in self.attachment_points]
gib_pos.sort()
hole_pos = [(x1 + x2) / 2 for x1, x2 in zip(gib_pos[:-1], gib_pos[1:])]
rigid = RigidFoil(-.15, .12)
r_flat = rigid.get_flattened(self.rib)
print(self.rib.rotation_matrix,
norm(self.rib.rotation_matrix.dot([2, 0, 0])))
Graph.Graphics([
Graph.Line(prof),
Graph.Line(self.rib.profile_2d.data * self.rib.chord),
Graph.Line(r_flat)
])
Graph.Graphics([
Graph.Line([self.rib.align(p, scale=False) for p in prof.data]),
Graph.Line([self.rib.align(p, scale=False) for p in r_flat]),
Graph.Line(self.rib.profile_3d.data)
])
def _get_flattened(self, rib):
max_segment = 0.005 # 5mm
profile = rib.profile_2d
profile_normvectors = PolyLine2D(profile.normvectors)
start = profile(self.start)
end = profile(self.end)
point_range = []
last_node = None
for p in profile[start:end]:
sign = -1 if p[1] > 0 else +1
if last_node is not None:
diff = norm(p - last_node) * rib.chord
if diff > max_segment:
segments = int(math.ceil(diff / max_segment))
point_range += list(
np.linspace(point_range[-1], sign * p[0],
segments))[1:]
else:
point_range.append(sign * p[0])
else:
point_range.append(sign * p[0])
last_node = p
indices = [profile(x) for x in point_range]
return [(profile[index] - profile_normvectors[index] * self.func(x)) *
rib.chord for index, x in zip(indices, point_range)]
def midrib_basic_cell(self, y, ballooning=True, arc_argument=True):
if y == 0: # left side
return self.prof1
elif y == 1: # right side
return self.prof2
else: # somewhere
#self._checkxvals()
midrib = []
for i in range(len(self.prof1.data)): # Arc -> phi(bal) -> r # oder so...
diff = self.prof1[i] - self.prof2[i]
if ballooning and self.ballooning_radius[i] > 0.:
if arc_argument:
d = 0.5 - math.sin(self.ballooning_phi[i] * (0.5 - y)) / math.sin(self.ballooning_phi[i])
h = math.cos(self.ballooning_phi[i] * (1 - 2 * y)) - self.ballooning_cos_phi[i]
#h = math.sqrt(1 - (norm(diff) * (0.5 - d) / self._radius[i]) ** 2)
#h -= self._cosphi[i] # cosphi2-cosphi
else:
d = y
h = math.sqrt(1 - (norm(diff) * (0.5 - y) / self.ballooning_radius[i]) ** 2)
h -= self.ballooning_cos_phi[i] # cosphi2-cosphi
else: # Without ballooning
d = y
h = 0.
midrib.append(self.prof1[i] - diff * d + self.normvectors[i] * h * self.ballooning_radius[i])
return Profile3D(midrib)
def get_length(self, cell):
rib1 = cell.rib1
rib2 = cell.rib2
left = rib1.profile_3d[rib1.profile_2d(self.left)]
right = rib2.profile_3d[rib2.profile_2d(self.right)]
return norm(left - right)
def ballooning_radius(self):
radius = []
for i, phi in enumerate(self.ballooning_phi):
if round(phi, 5) > 0:
radius.append(norm(self.prof1.data[i] - self.prof2.data[i]) / (2*numpy.sin(phi)))
else:
radius.append(0)
return radius
def span(self):
span = 0.
front = self.get_spanwise()
last = front[0] * [0, 0, 1] # centerrib only halfed
for this in front[1:]:
span += norm((this - last) * [0, 1, 1])
last = this
return 2 * span
def ballooning_radius(self):
radius = []
for i, phi in enumerate(self.ballooning_phi):
if round(phi, 5) > 0:
radius.append(norm(self.prof1.data[i] - self.prof2.data[i]) / (2*numpy.sin(phi)))
else:
radius.append(0)
return radius
def calc_panel_geo(self):
for i in range(self.length):
self.panel.append(numpy.array([self.airfoil[i], self.airfoil[i + 1]]))
self.panel_mids.append((self.airfoil[i] + self.airfoil[i + 1]) / 2)
self.half_lenghts[i] = vector.norm(self.airfoil[i] - self.airfoil[i + 1]) / 2
self.panel_tangentials.append(self.panel[-1][1] - self.panel[-1][0])
self.panel_normals.append(vector.normalize([-self.panel_tangentials[-1][1], self.panel_tangentials[-1][0]]))
for i in range(self.wake_numpoints - 1):
self.wake_panels.append(numpy.array([self.wake[i], self.wake[i + 1]]))
def _douplet_const(self, point_j, panel):
point_i_1, point_i_2 = panel
t = point_i_2 - point_i_1
n_ = vector.normalize([t[1], -t[0]])
pn, s0 = numpy.linalg.solve(numpy.transpose(numpy.array([n_, t])), -point_i_1 + point_j)
l = vector.norm(t)
if pn == 0:
return 0
else:
return 1 / 2 / numpy.pi * (-numpy.arctan2(pn, (s0 - 1) * l) + numpy.arctan2(pn, s0 * l))
def _normalize(line, target_lengths):
new_line = [line[0]]
last_node = line[0]
segments = line.get_segments()
for segment, target_length in zip(segments, target_lengths):
scale = target_length / norm(segment)
last_node = last_node + scale * segment
new_line.append(last_node)
return PolyLine2D(new_line)
def noseindex(self):
p0 = self.data[0]
max = 0
noseindex = 0
for i, p1 in enumerate(self.data):
diff = norm(p1 - p0)
if diff > max:
noseindex = i
max = diff
return noseindex
def noseindex(self):
p0 = self.data[0]
max = 0
noseindex = 0
for i, p1 in enumerate(self.data):
diff = norm(p1 - p0)
if diff > max:
noseindex = i
max = diff
return noseindex
def draw(self, graphics):
cell, pointnums = super(Arrow, self).draw(graphics)
assert len(pointnums) == 2
arrow = vtk.vtkArrowSource()
p1, p2 = graphics.get_points(*pointnums)
transform = vtk.vtkTransform()
transform.Translate(p1)
length = norm(p2-p1)
transform.Scale(length, length, length)
pass
def test_extend_case_afterend(self):
#First Point further than the end
for thalist in self.vectors:
start = self.numpoints + random.random() * 50
leng = random.random() * 100 - 50
new = thalist.extend(start, leng)
leng2 = thalist.get_length(start, new)
self.assertAlmostEqual(abs(leng), leng2, 7,
"Failed for start=" + str(start) + " and leng=" + str(leng) +
"\nresult: i2=" + str(new) + " leng2=" + str(leng2) +
" dist=" + str(vector.norm(thalist[start] - thalist[new])))
def draw(self, graphics):
cell, pointnums = super(Arrow, self).draw(graphics)
assert len(pointnums) == 2
arrow = vtk.vtkArrowSource()
p1, p2 = graphics.get_points(*pointnums)
transform = vtk.vtkTransform()
transform.Translate(p1)
length = norm(p2-p1)
transform.Scale(length, length, length)
pass
def test_extend_total(self):
#Sum up the length of the list and check
for thalist in self.vectors:
total = 0
for i in range(len(thalist) - 2):
total += vector.norm(thalist[i] - thalist[i + 1])
# First Test:
i2 = thalist.extend(0, total)
self.assertAlmostEqual(i2, len(thalist) - 2)
# Second Test:
self.assertAlmostEqual(total, thalist.get_length(0, len(thalist) - 2))
def test_extend_case_afterend(self):
#First Point further than the end
for thalist in self.vectors:
start = self.numpoints + random.random() * 50
leng = random.random() * 100 - 50
new = thalist.extend(start, leng)
leng2 = thalist.get_length(start, new)
self.assertAlmostEqual(
abs(leng), leng2, 7,
"Failed for start=" + str(start) + " and leng=" + str(leng) +
"\nresult: i2=" + str(new) + " leng2=" + str(leng2) +
" dist=" + str(vector.norm(thalist[start] - thalist[new])))
def get_all(self):
gib_pos = [n.rib_pos for n in self.attachment_points]
gib_pos.sort()
hole_pos = [(x1 + x2) / 2 for x1, x2 in zip(gib_pos[:-1], gib_pos[1:])]
gibs = [self.get_gibus_arcs(y) for y in gib_pos]
holes = [self.get_hole(x, 0.4) for x in hole_pos]
rigid = self.get_rigid(-.15, .13)
p = self.rib.profile_2d
print(max([norm(p[0] - p2) for p2 in p]), self.rib.chord)
return [Graph.Line(self.rib.profile_3d.data)] + gibs + holes + [rigid]
def test_extend_total(self):
#Sum up the length of the list and check
for thalist in self.vectors:
total = 0
for i in range(len(thalist) - 2):
total += vector.norm(thalist[i] - thalist[i + 1])
# First Test:
i2 = thalist.extend(0, total)
self.assertAlmostEqual(i2, len(thalist) - 2)
# Second Test:
self.assertAlmostEqual(total,
thalist.get_length(0,
len(thalist) - 2))
def flatten_list(list1, list2):
index_left = index_right = 0
flat_left = [numpy.array([0, 0])]
flat_right = [numpy.array([norm(list1[0]-list2[0]), 0])]
# def which(i, j):
# diff = list1[i] - list2[j]
# return diff.dot(list1[i+1]-list1[i]+list2[j+1]-list2[j+1])
while True:
#while which(index_left, index_right) <= 0 and index_left < len(list1) - 2: # increase left_index
if index_left < len(list1) -1:
flat_left.append(point2d(list1[index_left], flat_left[index_left],
list2[index_right], flat_right[index_right],
list1[index_left + 1]))
index_left += 1
#while which(index_left, index_right) >= 0 and index_right < len(list2) - 2: # increase right_index
if index_right < len(list2) -1:
flat_right.append(point2d(list1[index_left], flat_left[index_left],
list2[index_right], flat_right[index_right],
list2[index_right + 1]))
index_right += 1
if index_left == len(list1) - 1 and index_right == len(list2) - 1:
break
# while index_left < len(list1) - 1:
# flat_left.append(point2d(list1[index_left], flat_left[index_left],
# list2[index_right], flat_right[index_right],
# list1[index_left + 1]))
# index_left += 1
#
# while index_right < len(list2) - 1:
# flat_right.append(point2d(list1[index_left], flat_left[index_left],
# list2[index_right], flat_right[index_right],
# list2[index_right + 1]))
# index_right += 1
return Vectorlist2D(flat_left), Vectorlist2D(flat_right)
def projection(self):
if not self._xvekt or not self._yvekt or not self._diff:
p1 = self.data[0]
diff_len = nose_index = 0
diff = [p - p1 for p in self.data]
for i in range(len(self.data)):
thisdiff = norm(diff[i])
if thisdiff > diff_len:
nose_index = i
diff_len = thisdiff
xvect = normalize(diff[nose_index])
yvect = numpy.array([0, 0, 0])
for i in range(len(diff)):
sign = 1 - 2 * (i > nose_index)
yvect = yvect + sign * (diff[i] - xvect * xvect.dot(diff[i]))
self.xvect = xvect
self.yvect = normalize(yvect)
self._diff = diff
self.noseindex = nose_index
def flatten_list(list1, list2):
index_left = index_right = 0
flat_left = [numpy.array([0, 0])]
flat_right = [numpy.array([norm(list1[0]-list2[0]), 0])]
# def which(i, j):
# diff = list1[i] - list2[j]
# return diff.dot(list1[i+1]-list1[i]+list2[j+1]-list2[j+1])
while True:
#while which(index_left, index_right) <= 0 and index_left < len(list1) - 2: # increase left_index
if index_left < len(list1) - 1:
flat_left.append(point2d(list1[index_left], flat_left[index_left],
list2[index_right], flat_right[index_right],
list1[index_left + 1]))
index_left += 1
#while which(index_left, index_right) >= 0 and index_right < len(list2) - 2: # increase right_index
if index_right < len(list2) - 1:
flat_right.append(point2d(list1[index_left], flat_left[index_left],
list2[index_right], flat_right[index_right],
list2[index_right + 1]))
index_right += 1
if index_left == len(list1) - 1 and index_right == len(list2) - 1:
break
# while index_left < len(list1) - 1:
# flat_left.append(point2d(list1[index_left], flat_left[index_left],
# list2[index_right], flat_right[index_right],
# list1[index_left + 1]))
# index_left += 1
#
# while index_right < len(list2) - 1:
# flat_right.append(point2d(list1[index_left], flat_left[index_left],
# list2[index_right], flat_right[index_right],
# list2[index_right + 1]))
# index_right += 1
return Vectorlist2D(flat_left), Vectorlist2D(flat_right)
def normalize(self):
"""
Normalize the airfoil.
This routine does:
*Put the nose back to (0,0)
*De-rotate airfoil
*Reset its length to 1
"""
#to normalize do: put nose to (0,0), rotate to fit (1,0), normalize to (1,0)
p1 = self.data[0]
dmax = 0.
nose = p1
for i in self.data:
temp = norm(i - p1)
if temp > dmax:
dmax = temp
nose = i
diff = p1 - nose
sin = diff.dot([0, -1]) / dmax # Angle: a.b=|a|*|b|*sin(alpha)
cos = numpy.sqrt(1 - sin ** 2)
matrix = numpy.array([[cos, -sin], [sin, cos]]) / dmax # de-rotate and scale
self.data = numpy.array([matrix.dot(i - nose) for i in self.data])
def normalize(self):
"""
Normalize the airfoil.
This routine does:
*Put the nose back to (0,0)
*De-rotate airfoil
*Reset its length to 1
"""
#to normalize do: put nose to (0,0), rotate to fit (1,0), normalize to (1,0)
p1 = self.data[0]
dmax = 0.
nose = p1
for i in self.data:
temp = norm(i - p1)
if temp > dmax:
dmax = temp
nose = i
diff = p1 - nose
sin = diff.dot([0, -1]) / dmax # Angle: a.b=|a|*|b|*sin(alpha)
cos = numpy.sqrt(1 - sin**2)
matrix = numpy.array([[cos, -sin], [sin, cos]
]) / dmax # de-rotate and scale
self.data = numpy.array([matrix.dot(i - nose) for i in self.data])
def length_no_sag(self):
return norm(self.upper_node.vec - self.lower_node.vec)
def area(self):
p1_1 = self.rib1.align([0, 0, 0])
p1_2 = self.rib1.align([1, 0, 0])
p2_1 = self.rib2.align([0, 0, 0])
p2_2 = self.rib2.align([1, 0, 0])
return 0.5 * (norm(numpy.cross(p1_2 - p1_1, p2_1 - p1_1)) + norm(numpy.cross(p2_2 - p2_1, p2_2 - p1_2)))
def length_projected(self):
return norm(self.lower_node.vec_proj - self.upper_node.vec_proj)
def length_projected(self):
return norm(self.lower_node.vec_proj - self.upper_node.vec_proj)
def drag_differential(self):
"""drag per meter"""
return 1 / 2 * self.type.cw * self.type.thickness * norm(self.v_inf) ** 2
def _insert_attachment_points(self, plotpart, attachment_points):
for attachment_point in attachment_points:
if hasattr(attachment_point, "cell"):
if attachment_point.cell != self.cell:
continue
cell_pos = attachment_point.cell_pos
elif hasattr(attachment_point, "rib"):
if attachment_point.rib not in self.cell.ribs:
continue
if attachment_point.rib == self.cell.rib1:
cell_pos = 0
align = ("left", "right")
elif attachment_point.rib == self.cell.rib2:
cell_pos = 1
cut_f_l = self.panel.cut_front["left"]
cut_f_r = self.panel.cut_front["right"]
cut_b_l = self.panel.cut_back["left"]
cut_b_r = self.panel.cut_back["right"]
cut_f = cut_f_l + cell_pos * (cut_f_r - cut_f_l)
cut_b = cut_b_l + cell_pos * (cut_b_r - cut_b_l)
if cut_f <= attachment_point.rib_pos <= cut_b:
rib_pos = attachment_point.rib_pos
left, right = self.get_point(rib_pos)
p1 = left + cell_pos * (right - left)
d = normalize(right - left) * 0.008 # 8mm
if cell_pos == 1:
p2 = p1 + d
else:
p2 = p1 - d
#p1, p2 = self.get_p1_p2(attachment_point.rib_pos, which)
plotpart.layers["marks"] += self.config.marks_attachment_point(
p1, p2)
plotpart.layers[
"L0"] += self.config.marks_laser_attachment_point(p1, p2)
if self.config.insert_attachment_point_text:
text_align = "left" if cell_pos > 0.7 else "right"
if text_align == "right":
d1 = norm(self.get_point(cut_f_l)[0] - left)
d2 = norm(self.get_point(cut_b_l)[0] - left)
else:
d1 = norm(self.get_point(cut_f_r)[1] - right)
d2 = norm(self.get_point(cut_b_r)[1] - right)
bl = self.ballooned[0]
br = self.ballooned[1]
text_height = 0.01 * 0.8
dmin = text_height + 0.001
if d1 < dmin and d2 + d1 > 2 * dmin:
offset = dmin - d1
ik = get_x_value(self.x_values, rib_pos)
left = bl[bl.extend(ik, offset)]
right = br[br.extend(ik, offset)]
elif d2 < dmin and d1 + d2 > 2 * dmin:
offset = dmin - d2
ik = get_x_value(self.x_values, rib_pos)
left = bl[bl.extend(ik, -offset)]
right = br[br.extend(ik, -offset)]
if self.config.layout_seperate_panels and self.panel.is_lower:
# rotated later
p2 = left
p1 = right
# text_align = text_align
else:
p1 = left
p2 = right
# text_align = text_align
plotpart.layers["text"] += Text(
" {} ".format(attachment_point.name),
p1,
p2,
size=0.01, # 1cm
align=text_align,
valign=0,
height=0.8).get_vectors()
def get_flattened_cell(self, midribs=10):
left, right = openglider.vector.projection.flatten_list(
self.prof1, self.prof2)
left_bal = left.copy()
right_bal = right.copy()
ballooning = [
self.ballooning[x] for x in self.rib1.profile_2d.x_values
]
for i in range(len(left)):
diff = (right[i] - left[i]) * ballooning[i] / 2
left_bal.data[i] -= diff
right_bal.data[i] += diff
def _normalize(line, target_lengths):
new_line = [line[0]]
last_node = line[0]
segments = line.get_segments()
for segment, target_length in zip(segments, target_lengths):
scale = target_length / norm(segment)
last_node = last_node + scale * segment
new_line.append(last_node)
return PolyLine2D(new_line)
#
left_bal_2 = _normalize(left_bal, left.get_segment_lengthes())
right_bal_2 = _normalize(right_bal, right.get_segment_lengthes())
right_bal_3 = right_bal_2.copy()
left_bal_3 = left_bal_2.copy()
debug_lines = []
debug_lines2 = []
for i in range(len(left_bal)):
diff = left_bal_2[i] - right_bal_2[i]
dist_new = norm(diff)
dist_orig = norm(left_bal[i] - right_bal[i])
diff_per_side = normalize(diff) * ((dist_new - dist_orig) / 2)
right_bal_2[i] += diff_per_side
left_bal_2[i] -= diff_per_side
debug_lines.append(PolyLine2D([left_bal_2[i], right_bal_2[i]]))
debug_lines2.append(PolyLine2D([left_bal[i], right_bal[i]]))
inner = []
for x in openglider.utils.linspace(0, 1, 2 + midribs):
l1 = left_bal * (1 - x)
l2 = right_bal * x
inner.append(l1.add(l2))
#ballooned = [left_bal, right_bal]
return {
"inner": inner,
"ballooned": [left_bal, right_bal],
"ballooned_new": [left_bal_2, right_bal_2],
"ballooned_new_copy": [left_bal_3, right_bal_3],
"debug": [left, right],
"debug_1": debug_lines,
"debug_2": debug_lines2
}
def span(self): # TODO: Maybe use mean length from (1,0), (0,0)
return norm((self.rib1.pos - self.rib2.pos) * [0, 1, 1])
def length_no_sag(self):
return norm(self.upper_node.vec - self.lower_node.vec)
def span(self):
return norm((self.rib1.pos - self.rib2.pos) * [0, 1, 1])
def drag_differential(self):
"""drag per meter"""
return 1 / 2 * self.type.cw * self.type.thickness * norm(self.v_inf)**2
def setUp(self, numpoints=100):
self.p1 = np.array([random.random(), random.random()])
self.d = np.array([random.random(), random.random()]) * 100
self.l = norm(self.d)
self.p2 = self.p1 + self.d