def _BuildRibs(self, ChordFactor, ScaleFactor):
"""Generates Ribs surface along the wingspan, given the general,
nondimensional parameters of the object (variations of chord length,
dihedral, etc.) and the two scaling factors.
Parameters
----------
ChordFactor - float
Factor againt which the standard shape is scaled in the chordwise
direction
ScaleFactor - float
Factor againt which the standard shape is scaled in the world
coordinates
Returns
-------
Ribs : TopoDS_Shape
The generated Ribs surface
"""
SectionsRibs = []
RibsFace = []
Step = (self.SegmentNoLoft) / (self.NoRibs - 1)
LEPointsR = self._GenerateLeadingEdge()
Eps = np.linspace(0, 1, self.SegmentNoLoft + 1)
SectionsRibs = [
self.AirfoilFunct(Eps[i], LEPointsR[i], self.ChordFunct,
ChordFactor, self.DihedralFunct,
self.TwistFunct).Curve
for i in xrange(0, self.SegmentNoLoft + 1, Step)
]
LESpar, TESpar, MIDSpar, StringerUp, StringerDown, PointsUp, PointsDown = self._BuildSpars(
self.ChordFactor, self.ScaleFactor)
# RIBS generated from segments
for i in range(0, self.NoRibs):
for ii in range(0, self.NoStiffners - 1):
SegUp = GC_MakeSegment(
PointsUp[ii + i * self.NoStiffners * (Step)],
PointsUp[ii + i * self.NoStiffners * (Step) + 1]).Value()
SegDown = GC_MakeSegment(
PointsDown[ii + i * self.NoStiffners * (Step) + 1],
PointsDown[ii + i * self.NoStiffners * (Step)]).Value()
SegSide1 = GC_MakeSegment(
PointsDown[ii + i * self.NoStiffners * (Step)],
PointsUp[ii + i * self.NoStiffners * (Step)]).Value()
SegSide2 = GC_MakeSegment(
PointsUp[ii + i * self.NoStiffners * (Step) + 1],
PointsDown[ii + i * self.NoStiffners * (Step) +
1]).Value()
EdgeSegUp = act.make_edge(SegUp)
EdgeSegDown = act.make_edge(SegDown)
EdgeSide1 = act.make_edge(SegSide1)
EdgeSide2 = act.make_edge(SegSide2)
WireRib = act.make_wire(
[EdgeSide1, EdgeSegUp, EdgeSide2, EdgeSegDown])
FaceRibi = act.make_face(WireRib)
if self.ScaleFactor != 1:
Origin = gp_Pnt(0., 0., 0.)
FaceRib = act.scale_uniformal(FaceRibi, Origin,
self.ScaleFactor)
RibsFace.append(FaceRib)
return SectionsRibs, RibsFace
def _BuildPanels(self, ChordFactor, ScaleFactor):
LESpar, TESpar, MIDSpar, StringerUp, StringerDown, PointsUp, PointsDown = self._BuildSpars(
self.ChordFactor, self.ScaleFactor)
PanelUp = []
PanelDown = []
cont = 1
for ii in range(0, len(PointsUp) - self.NoStiffners - 1):
if cont == self.NoStiffners:
cont = 0
else:
cont = cont
# Panel from segments
SegH1 = GC_MakeSegment(
PointsUp[ii], PointsUp[ii + self.NoStiffners]).Value()
SegH2 = GC_MakeSegment(PointsUp[ii + 1],
PointsUp[ii + self.NoStiffners +
1]).Value()
SegV1 = GC_MakeSegment(PointsUp[ii], PointsUp[ii + 1]).Value()
SegV2 = GC_MakeSegment(PointsUp[ii + self.NoStiffners],
PointsUp[ii + self.NoStiffners +
1]).Value()
EdgeHUp1 = act.make_edge(SegH1)
EdgeHUp2 = act.make_edge(SegH2)
EdgeVUp1 = act.make_edge(SegV1)
EdgeVUp2 = act.make_edge(SegV2)
WirePanelUp = act.make_wire(
[EdgeHUp1, EdgeVUp1, EdgeHUp2, EdgeVUp2])
PanelUpi = act.make_face(WirePanelUp)
# In this way the pannel will be ordered in alternance between upper and lower surface
SegH1 = GC_MakeSegment(
PointsDown[ii], PointsDown[ii + self.NoStiffners]).Value()
SegH2 = GC_MakeSegment(PointsDown[ii + 1],
PointsDown[ii + self.NoStiffners +
1]).Value()
SegV1 = GC_MakeSegment(PointsDown[ii],
PointsDown[ii + 1]).Value()
SegV2 = GC_MakeSegment(PointsDown[ii + self.NoStiffners],
PointsDown[ii + self.NoStiffners +
1]).Value()
EdgeHUp1 = act.make_edge(SegH1)
EdgeHUp2 = act.make_edge(SegH2)
EdgeVUp1 = act.make_edge(SegV1)
EdgeVUp2 = act.make_edge(SegV2)
WirePanelDown = act.make_wire(
[EdgeHUp1, EdgeVUp1, EdgeHUp2, EdgeVUp2])
PanelDowni = act.make_face(WirePanelDown)
if self.ScaleFactor != 1:
Origin = gp_Pnt(0., 0., 0.)
PanelUpi = act.scale_uniformal(PanelUpi, Origin,
self.ScaleFactor)
PanelDowni = act.scale_uniformal(PanelDowni, Origin,
self.ScaleFactor)
PanelUp.append(PanelUpi)
PanelDown.append(PanelDowni)
cont = cont + 1
return PanelUp, PanelDown
def _BuildSpars(self, ChordFactor, ScaleFactor):
LE = self._GenerateLeadingEdge()
self.NoStiffners = self.NoStiffnersLE + self.NoStiffnersTE
SectionsProfiles = []
SparLEFullWing = []
SparTEFullWing = []
SparMIDFullWing = []
SparLEup = []
SparLEdown = []
SparMIDup = []
SparMIDdown = []
SparTEup = []
SparTEdown = []
planeStiffEps = []
PStiffUpFullWing = []
PStiffDownFullWing = []
StringerUpFullWing = []
StringerDownFullWing = []
EpsS = np.linspace(0, 1, self.SegmentNoLoft + 1)
SectionsProfiles = [
self.AirfoilFunct(EpsS[d], LE[d], self.ChordFunct, ChordFactor,
self.DihedralFunct, self.TwistFunct).Curve
for d in xrange(self.SegmentNoLoft + 1)
]
# Stringers generation
h = 0
cont3 = 0
PointsUp = []
PointsDown = []
PointsMIDup = []
PointsMIDdown = []
for SecR in SectionsProfiles:
ChordLenght = ((ChordFactor * self.ChordFunct(EpsS[h])) /
np.cos(np.radians(self.TwistFunct(EpsS[h]))))
LELengthX = LE[h, 0]
LEplanePositionX = (self.PositionLESpar * ChordLenght) * np.cos(
self.TwistFunct(EpsS[h])) + LELengthX
TEplanePositionX = (self.PositionTESpar * ChordLenght) * np.cos(
self.TwistFunct(EpsS[h])) + LELengthX
MIDplanePositionX = (self.PositionMIDSpar * ChordLenght) * np.cos(
self.TwistFunct(EpsS[h])) + LELengthX
planeLEi = Geom_Plane(
gp_Pln(gp_Pnt(LEplanePositionX, 0., 0.),
gp_Dir(gp_Vec(gp_Pnt(0., 0., 0.), gp_Pnt(1., 0., 0.)))))
planeMIDi = Geom_Plane(
gp_Pln(gp_Pnt(MIDplanePositionX, 0., 0.),
gp_Dir(gp_Vec(gp_Pnt(0., 0., 0.), gp_Pnt(1., 0., 0.)))))
planeTEi = Geom_Plane(
gp_Pln(gp_Pnt(TEplanePositionX, 0., 0.),
gp_Dir(gp_Vec(gp_Pnt(0., 0., 0.), gp_Pnt(1., 0., 0.)))))
# planeLEi.Rotate(gp_OY(), -np.radians(self.TwistFunct(EpsS[h])))
# planeMIDi.Rotate(gp_OY(), -np.radians(self.TwistFunct(EpsS[h])))
# planeTEi.Rotate(gp_OY(), -np.radians(self.TwistFunct(EpsS[h])))
SegmentStiffLE = (MIDplanePositionX -
LEplanePositionX) / (self.NoStiffnersLE - 1)
SegmentStiffTE = (TEplanePositionX -
MIDplanePositionX) / (self.NoStiffnersTE)
NoStiffners = self.NoStiffnersLE + self.NoStiffnersTE
PStiffUpi = []
PStiffDowni = []
PosStiffiEps = LEplanePositionX
for g in xrange(NoStiffners):
planeStiffEps = Geom_Plane(
gp_Pln(
gp_Pnt(PosStiffiEps, 0., 0.),
gp_Dir(gp_Vec(gp_Pnt(0., 0., 0.), gp_Pnt(1., 0.,
0.)))))
StiffiEps = GeomAPI_IntCS(SecR, planeStiffEps.GetHandle())
with act.assert_isdone(StiffiEps,
'failed to calculate intersection'):
nb_results = StiffiEps.NbPoints()
if nb_results == 1:
return StiffiEps.Point(1)
#print("One point intersection")
elif nb_results >= 1:
#print("More than one intersection point")
PStiff = []
for i in range(1, nb_results + 1):
PStiff.append(StiffiEps.Point(i))
else:
return None
PStiffUpi.append(PStiff[0])
PStiffDowni.append(PStiff[nb_results - 1])
if g <= self.NoStiffnersLE - 2:
PosStiffiEps = PosStiffiEps + SegmentStiffLE
else:
PosStiffiEps = PosStiffiEps + SegmentStiffTE
PointsUp.append(PStiff[0])
PointsDown.append(PStiff[nb_results - 1])
SparLEi = GeomAPI_IntCS(SecR, planeLEi.GetHandle())
with act.assert_isdone(SparLEi,
'failed to calculate intersection'):
nb_results = SparLEi.NbPoints()
#print(nb_results)
if nb_results == 1:
return SparLEi.Point(1)
#print("One point intersection")
elif nb_results >= 1:
#print("More than one intersection point")
PLE = []
for i in range(1, nb_results + 1):
PLE.append(SparLEi.Point(i))
else:
return None
SegLE = GC_MakeSegment(PLE[0], PLE[nb_results - 1]).Value()
SparMIDi = GeomAPI_IntCS(SecR, planeMIDi.GetHandle())
with act.assert_isdone(SparMIDi,
'failed to calculate intersection'):
nb_results = SparMIDi.NbPoints()
#print(nb_results)
if nb_results == 1:
return SparMIDi.Point(1)
#print("One point intersection")
elif nb_results >= 1:
#print("More than one intersection point")
PMID = []
for i in range(1, nb_results + 1):
PMID.append(SparMIDi.Point(i))
else:
return None
SegMID = GC_MakeSegment(PMID[0], PMID[nb_results - 1]).Value()
PointsMIDup.append(PMID[0])
PointsMIDdown.append(PMID[nb_results - 1])
SparTEi = GeomAPI_IntCS(SecR, planeTEi.GetHandle())
with act.assert_isdone(SparTEi,
'failed to calculate intersection'):
nb_results = SparTEi.NbPoints()
#print(nb_results)
if nb_results == 1:
return SparTEi.Point(1)
#print("One point intersection")
elif nb_results >= 1:
#print("More than one intersection point")
PTE = []
for i in range(1, nb_results + 1):
PTE.append(SparTEi.Point(i))
else:
return None
SegTE = GC_MakeSegment(PTE[0], PTE[nb_results - 1]).Value()
#print(len(SparMIDdown))
#print(len(SparMIDup))
#print(len(SparLEup))
#print(len(SparLEdown))
SparLEFullWing.append(SegLE)
SparMIDFullWing.append(SegMID)
SparTEFullWing.append(SegTE)
SparLEup.append(PLE[0])
SparLEdown.append(PLE[nb_results - 1])
SparMIDup.append(PMID[0])
#print(PMID[nb_results-1])
SparMIDdown.append(PMID[nb_results - 1])
SparTEup.append(PTE[0])
SparTEdown.append(PTE[nb_results - 1])
PStiffUpFullWing.append(PStiffUpi)
PStiffDownFullWing.append(PStiffDowni)
cont3 = cont3 + 1
h = h + 1
# Method to create spars - VIA SEGMENTS
#LE
LoftLESparFullWing = []
for iii in xrange(0,
len(PointsUp) - 2 * (self.NoStiffners - 1),
self.NoStiffners):
SegUp = GC_MakeSegment(PointsUp[iii],
PointsUp[iii + self.NoStiffners]).Value()
SegDown = GC_MakeSegment(PointsDown[iii + self.NoStiffners],
PointsDown[iii]).Value()
SegSide1 = GC_MakeSegment(PointsDown[iii], PointsUp[iii]).Value()
SegSide2 = GC_MakeSegment(PointsUp[iii + self.NoStiffners],
PointsDown[iii +
self.NoStiffners]).Value()
EdgeSegUp = act.make_edge(SegUp)
EdgeSegDown = act.make_edge(SegDown)
EdgeSide1 = act.make_edge(SegSide1)
EdgeSide2 = act.make_edge(SegSide2)
WireSparLE = act.make_wire(
[EdgeSide1, EdgeSegUp, EdgeSide2, EdgeSegDown])
FaceSparLEi = act.make_face(WireSparLE)
if self.ScaleFactor != 1:
Origin = gp_Pnt(0., 0., 0.)
FaceSparLE = act.scale_uniformal(FaceSparLEi, Origin,
self.ScaleFactor)
LoftLESparFullWing.append(FaceSparLE)
#MID
LoftMIDSparFullWing = []
for iii in xrange(0, self.SegmentNoLoft):
SegUp = GC_MakeSegment(PointsMIDup[iii],
PointsMIDup[iii + 1]).Value()
SegDown = GC_MakeSegment(PointsMIDdown[iii + 1],
PointsMIDdown[iii]).Value()
SegSide1 = GC_MakeSegment(PointsMIDdown[iii],
PointsMIDup[iii]).Value()
SegSide2 = GC_MakeSegment(PointsMIDup[iii + 1],
PointsMIDdown[iii + 1]).Value()
EdgeSegUp = act.make_edge(SegUp)
EdgeSegDown = act.make_edge(SegDown)
EdgeSide1 = act.make_edge(SegSide1)
EdgeSide2 = act.make_edge(SegSide2)
WireSparMID = act.make_wire(
[EdgeSide1, EdgeSegUp, EdgeSide2, EdgeSegDown])
FaceSparMIDi = act.make_face(WireSparMID)
if self.ScaleFactor != 1:
Origin = gp_Pnt(0., 0., 0.)
FaceSparMID = act.scale_uniformal(FaceSparMIDi, Origin,
self.ScaleFactor)
LoftMIDSparFullWing.append(FaceSparMID)
#TE
LoftTESparFullWing = []
for iii in xrange(self.NoStiffners - 1,
len(PointsUp) - (self.NoStiffners),
self.NoStiffners):
SegUp = GC_MakeSegment(PointsUp[iii],
PointsUp[iii + self.NoStiffners]).Value()
SegDown = GC_MakeSegment(PointsDown[iii + self.NoStiffners],
PointsDown[iii]).Value()
SegSide1 = GC_MakeSegment(PointsDown[iii], PointsUp[iii]).Value()
SegSide2 = GC_MakeSegment(PointsUp[iii + self.NoStiffners],
PointsDown[iii +
self.NoStiffners]).Value()
EdgeSegUp = act.make_edge(SegUp)
EdgeSegDown = act.make_edge(SegDown)
EdgeSide1 = act.make_edge(SegSide1)
EdgeSide2 = act.make_edge(SegSide2)
WireSparTE = act.make_wire(
[EdgeSide1, EdgeSegUp, EdgeSide2, EdgeSegDown])
FaceSparTEi = act.make_face(WireSparTE)
if self.ScaleFactor != 1:
Origin = gp_Pnt(0., 0., 0.)
FaceSparTE = act.scale_uniformal(FaceSparTEi, Origin,
self.ScaleFactor)
LoftTESparFullWing.append(FaceSparTE)
for g in range(self.NoStiffners):
for gg in range(self.SegmentNoLoft):
SegStringerUp = GC_MakeSegment(
PointsUp[gg * self.NoStiffners + g],
PointsUp[gg * self.NoStiffners + g +
self.NoStiffners]).Value()
SegStringerDown = GC_MakeSegment(
PointsDown[gg * self.NoStiffners + g],
PointsDown[gg * self.NoStiffners + g +
self.NoStiffners]).Value()
EdgeUp = act.make_edge(SegStringerUp)
EdgeDown = act.make_edge(SegStringerDown)
WireStringUp = act.make_wire(EdgeUp)
WireStringDown = act.make_wire(EdgeDown)
if self.ScaleFactor != 1:
Origin = gp_Pnt(0., 0., 0.)
StrUpFullWingi = act.scale_uniformal(
WireStringUp, Origin, self.ScaleFactor)
StrDownFullWingi = act.scale_uniformal(
WireStringDown, Origin, self.ScaleFactor)
#print('hello')
#print(self.ScaleFactor)
StringerUpFullWing.append(StrUpFullWingi)
StringerDownFullWing.append(StrDownFullWingi)
return LoftLESparFullWing, LoftTESparFullWing, LoftMIDSparFullWing, StringerUpFullWing, StringerDownFullWing, PointsUp, PointsDown
