def createHTP(CPACSObj, id, xRoot, zRoot, tcRoot, tcTip, cRoot, cTip, span, phiLE, dihedral, LoD=0, location=True):
if LoD == WING_LOD.NONE:
return
# just for now
cpacsPath = '/cpacs/vehicles/aircraft/model/wings/wing[' + id + ']'
# the next line is the one to use later on
# cpacsPath = '/cpacs/vehicles/aircraft/model[model]/wings/wing[' + self.id + ']'
# get the wing object from given cpacs path
myWing = getObjfromXpath(CPACSObj, cpacsPath)
myWing.set_name(stringBaseType(valueOf_='htp'))
strUID = createHeader(myWing, id)
myWing.set_symmetry('x-z-plane')
if location:
myWing.set_parentUID(stringUIDBaseType(isLink=True, valueOf_='fuselage'))
createTransformation(myWing, 'absGlobal', xRoot, 0., zRoot)
else:
myWing.set_parentUID(stringUIDBaseType(isLink=True, valueOf_='vtp'))
createTransformation(myWing, 'absGlobal', xRoot, 0., zRoot)
# call corresponding wing creation method
if LoD == WING_LOD.SINGLE:
createTrapezoidWing(myWing, id, tcTip, tcRoot, cTip, cRoot, span, phiLE, dihedral, 0., strUID)
if not location:
createWingWingAttachment(myWing.get_componentSegments().get_componentSegment()[0], strUID, targetUID='vtp_Cseg', typeOfSeg='ttail')
def createHTP(CPACSObj,
id,
xRoot,
zRoot,
tcRoot,
tcTip,
cRoot,
cTip,
span,
phiLE,
dihedral,
LoD=0,
location=True):
if LoD == WING_LOD.NONE:
return
# just for now
cpacsPath = '/cpacs/vehicles/aircraft/model/wings/wing[' + id + ']'
# the next line is the one to use later on
# cpacsPath = '/cpacs/vehicles/aircraft/model[model]/wings/wing[' + self.id + ']'
# get the wing object from given cpacs path
myWing = getObjfromXpath(CPACSObj, cpacsPath)
myWing.set_name(stringBaseType(valueOf_='htp'))
strUID = createHeader(myWing, id)
myWing.set_symmetry('x-z-plane')
if location:
myWing.set_parentUID(
stringUIDBaseType(isLink=True, valueOf_='fuselage'))
createTransformation(myWing, 'absGlobal', xRoot, 0., zRoot)
else:
myWing.set_parentUID(stringUIDBaseType(isLink=True, valueOf_='vtp'))
createTransformation(myWing, 'absGlobal', xRoot, 0., zRoot)
# call corresponding wing creation method
if LoD == WING_LOD.SINGLE:
createTrapezoidWing(myWing, id, tcTip, tcRoot, cTip, cRoot, span,
phiLE, dihedral, 0., strUID)
if not location:
createWingWingAttachment(
myWing.get_componentSegments().get_componentSegment()[0],
strUID,
targetUID='vtp_Cseg',
typeOfSeg='ttail')
def createVTP(CPACSObj,
id,
xRoot,
zRoot,
tcRoot,
tcTip,
cRoot,
cTip,
span,
phiLE,
LoD=0):
if LoD == WING_LOD.NONE:
return
# just for now
cpacsPath = '/cpacs/vehicles/aircraft/model/wings/wing[' + id + ']'
# the next line is the one to use later on
# cpacsPath = '/cpacs/vehicles/aircraft/model[model]/wings/wing[' + self.id + ']'
# get the wing object from given cpacs path
myWing = getObjfromXpath(CPACSObj, cpacsPath)
myWing.set_name(stringBaseType(valueOf_='vtp'))
myWing.set_parentUID(stringUIDBaseType(isLink=True, valueOf_='fuselage'))
strUID = createHeader(myWing, id)
# rotate vertical tail to correct orientation
createTransformation(myWing, 'absGlobal', xRoot, 0., zRoot, 1., 1., 1.,
90., 0., 0.)
# As the vtp is not symmetrical span values must be dubbled for conversion
span = span * 2
# call corresponding wing creation method
if LoD == WING_LOD.SINGLE:
createTrapezoidWing(myWing,
id,
tcRoot,
tcTip,
cTip,
cRoot,
span,
phiLE,
dihedral=0,
twist=0.,
strUID=strUID)
def createWing(CPACSObj=None, zeroWing=None, id="1", LoD=0.):
"""
This function triggers the different export modes of the wing depending on the desired
level of detail.
Options include a single trapezoid, double trapezoid, advanced double trapezoid (that includes
a rectangular center fuselage section) and a strut-braced wing.
Please note, these are the internal guts of VAMPzero's CPACS export. A lot of the code
here is experimental and furthermore highly chaotic. In case of emergency contact Daniel or Jonas.
:param CPACSObj: The overall CPACS object of the export
:param zeroWing: The instance of the wing.
:param id: The id of the wing, mostly sth. like wing
:param LoD: The level of detail of the desired input.
:return: CPACSObj including a new wing
"""
if LoD == WING_LOD.NONE:
return
# just for now
cpacsPath = '/cpacs/vehicles/aircraft/model/wings/wing[' + id + ']'
# the next line is the one to use later on
# cpacsPath = '/cpacs/vehicles/aircraft/model[model]/wings/wing[' + self.id + ']'
# get the wing object from given cpacs path
cpacsWing = getObjfromXpath(CPACSObj, cpacsPath)
strUID = createHeader(cpacsWing, id)
cpacsWing.set_symmetry('x-z-plane')
cpacsWing.set_name(stringBaseType(valueOf_='wing'))
cpacsWing.set_parentUID(stringUIDBaseType(isLink=True,
valueOf_='fuselage'))
xRoot = zeroWing.xRoot.getValue()
zRoot = zeroWing.zRoot.getValue()
cRoot = zeroWing.cRoot.getValue()
cTip = zeroWing.cTip.getValue()
span = zeroWing.span.getValue()
dfus = zeroWing.aircraft.fuselage.dfus.getValue()
phiLE = zeroWing.phiLE.getValue()
dihedral = zeroWing.dihedral.getValue()
twist = zeroWing.twist.getValue()
Sref = zeroWing.refArea.getValue()
xMAC25 = zeroWing.xMAC25.getValue()
tcRoot = zeroWing.airfoilr.tc.getValue()
tcTip = zeroWing.airfoilt.tc.getValue()
try:
etakf = zeroWing.etaKink.getValue()
yFus = zeroWing.yFuselage.getValue()
etaEng = zeroWing.etaEngine.getValue()
etaFus = yFus / span * 2.
except AttributeError:
pass #As not all components that call this method have a kink
try:
yRoot = zeroWing.yRoot.getValue()
except AttributeError:
pass #As not all components that call this method have a kink
createTransformation(cpacsWing, 'absGlobal', xRoot, 0., zRoot)
# call corresponding wing creation method
if LoD == WING_LOD.SINGLE:
createTrapezoidWing(cpacsWing, id, tcRoot, tcTip, cTip, cRoot, span,
phiLE, dihedral, twist, strUID)
elif LoD == WING_LOD.DOUBLE:
createDoubleTrapezoidWing(cpacsWing, id, cTip, cRoot, span, Sref,
phiLE, dihedral, twist, xMAC25, etakf,
strUID)
elif LoD == WING_LOD.ADVDOUBLE:
createAdvDoubleTrapezoidWing(cpacsWing, id, cTip, cRoot, span, Sref,
dfus, phiLE, dihedral, twist, xMAC25,
etakf, strUID, yFus, xRoot, etaEng,
tcRoot, tcTip)
elif LoD == WING_LOD.UCAV:
createUCAVWing(cpacsWing, id, cTip, cRoot, span, Sref, phiLE, dihedral,
etakf, strUID)
elif LoD == WING_LOD.SBW:
print "dihedral", dihedral
etaStrut = zeroWing.aircraft.strut.etaStrut.getValue()
createStrutBracedWing(cpacsWing,
id=id,
cTip=cTip,
cRoot=cRoot,
span=span,
Sref=Sref,
phiLE=phiLE,
dihedral=dihedral,
twist=twist,
xMAC25=xMAC25,
etaFus=etaFus,
etaStrut=etaStrut,
tcRoot=tcRoot,
tcTip=tcTip,
xRoot=xRoot,
strUID=strUID)
elif LoD == WING_LOD.STRUT:
etaStrut = zeroWing.aircraft.strut.etaStrut.getValue()
createStrut(cpacsWing,
id=id,
cTip=cTip,
cRoot=cRoot,
span=span,
phiLE=phiLE,
dihedral=dihedral,
tcRoot=tcRoot,
tcTip=tcTip,
xRoot=xRoot,
yRoot=yRoot,
twist=twist,
etaStrut=etaStrut,
strUID=strUID)
def createWing(CPACSObj = None, zeroWing = None, id="1", LoD = 0.):
"""
This function triggers the different export modes of the wing depending on the desired
level of detail.
Options include a single trapezoid, double trapezoid, advanced double trapezoid (that includes
a rectangular center fuselage section) and a strut-braced wing.
Please note, these are the internal guts of VAMPzero's CPACS export. A lot of the code
here is experimental and furthermore highly chaotic. In case of emergency contact Daniel or Jonas.
:param CPACSObj: The overall CPACS object of the export
:param zeroWing: The instance of the wing.
:param id: The id of the wing, mostly sth. like wing
:param LoD: The level of detail of the desired input.
:return: CPACSObj including a new wing
"""
if LoD == WING_LOD.NONE:
return
# just for now
cpacsPath = '/cpacs/vehicles/aircraft/model/wings/wing[' + id + ']'
# the next line is the one to use later on
# cpacsPath = '/cpacs/vehicles/aircraft/model[model]/wings/wing[' + self.id + ']'
# get the wing object from given cpacs path
cpacsWing = getObjfromXpath(CPACSObj, cpacsPath)
strUID = createHeader(cpacsWing, id)
cpacsWing.set_symmetry('x-z-plane')
cpacsWing.set_name(stringBaseType(valueOf_='wing'))
cpacsWing.set_parentUID(stringUIDBaseType(isLink=True, valueOf_='fuselage'))
xRoot = zeroWing.xRoot.getValue()
zRoot = zeroWing.zRoot.getValue()
cRoot = zeroWing.cRoot.getValue()
cTip = zeroWing.cTip.getValue()
span = zeroWing.span.getValue()
dfus = zeroWing.aircraft.fuselage.dfus.getValue()
phiLE = zeroWing.phiLE.getValue()
dihedral = zeroWing.dihedral.getValue()
twist = zeroWing.twist.getValue()
Sref = zeroWing.refArea.getValue()
xMAC25 = zeroWing.xMAC25.getValue()
tcRoot = zeroWing.airfoilr.tc.getValue()
tcTip = zeroWing.airfoilt.tc.getValue()
try:
etakf = zeroWing.etaKink.getValue()
yFus = zeroWing.yFuselage.getValue()
etaEng = zeroWing.etaEngine.getValue()
etaFus = yFus/span*2.
except AttributeError:
pass #As not all components that call this method have a kink
try:
yRoot = zeroWing.yRoot.getValue()
except AttributeError:
pass #As not all components that call this method have a kink
createTransformation(cpacsWing, 'absGlobal', xRoot, 0., zRoot)
# call corresponding wing creation method
if LoD == WING_LOD.SINGLE:
createTrapezoidWing(cpacsWing, id, tcRoot, tcTip, cTip, cRoot, span, phiLE, dihedral, twist, strUID)
elif LoD == WING_LOD.DOUBLE:
createDoubleTrapezoidWing(cpacsWing, id, cTip, cRoot, span, Sref, phiLE, dihedral, twist, xMAC25, etakf, strUID)
elif LoD == WING_LOD.ADVDOUBLE:
createAdvDoubleTrapezoidWing(cpacsWing, id, cTip, cRoot, span, Sref, dfus, phiLE, dihedral, twist, xMAC25, etakf, strUID, yFus, xRoot, etaEng, tcRoot, tcTip)
elif LoD == WING_LOD.UCAV:
createUCAVWing(cpacsWing, id, cTip, cRoot, span, Sref, phiLE, dihedral, etakf, strUID)
elif LoD == WING_LOD.SBW:
etaStrut = zeroWing.aircraft.strut.etaStrut.getValue()
createStrutBracedWing(cpacsWing, id=id, cTip=cTip, cRoot=cRoot, span=span, Sref=Sref, phiLE=phiLE, dihedral=dihedral, twist=twist, xMAC25=xMAC25, etaFus=etaFus, etaStrut=etaStrut, tcRoot=tcRoot, tcTip=tcTip, xRoot=xRoot, strUID=strUID)
elif LoD == WING_LOD.SBWStraight:
etaStrut = zeroWing.aircraft.strut.etaStrut.getValue()
createStraightStrutBracedWing(cpacsWing, id=id, cTip=cTip, cRoot=cRoot, span=span, Sref=Sref, phiLE=phiLE, dihedral=dihedral, twist=twist, xMAC25=xMAC25, etaFus=etaFus, etaStrut=etaStrut, tcRoot=tcRoot, tcTip=tcTip, xRoot=xRoot, strUID=strUID)
elif LoD == WING_LOD.STRUT:
etaStrut = zeroWing.aircraft.strut.etaStrut.getValue()
createStrut(cpacsWing, id=id, cTip=cTip, cRoot=cRoot, span=span, phiLE=phiLE, dihedral=dihedral, tcRoot=tcRoot, tcTip=tcTip, xRoot=xRoot, yRoot=yRoot, twist=twist, etaStrut=etaStrut, strUID=strUID)