def cpacsExport(self, CPACSObj):
'''
this methods exports all parameters nested in the component. Nested Components will be called as well.
cpacsPath must be filled
:Author: Jonas Jepsen
:param CPACSObj: the CPACS object holding the data for export
'''
# self.LoD.setValue(1) # level of detail [0,1]
if self.location.getValue():
xRoot = self.xRoot.getValue()
zRoot = self.zRoot.getValue()
else:
vtp_span = self.aircraft.vtp.span.getValue()
vtp_phiLE = (self.aircraft.vtp.phiLE.getValue()) * pi / 180.
xRoot = tan(vtp_phiLE) * vtp_span
try:
xRoot = xRoot.real
except:
pass
zRoot = vtp_span
createHTP(CPACSObj, self.id, xRoot, zRoot, self.airfoilr.tc.getValue(),
self.airfoilt.tc.getValue(), self.cRoot.getValue(),
self.cTip.getValue(), self.span.getValue(),
self.phiLE.getValue(), self.dihedral.getValue(),
self.LoD.getValue(), self.location.getValue())
super(wing, self).cpacsExport(CPACSObj)
def cpacsExport(self, CPACSObj):
'''
this methods exports all parameters nested in the component. Nested Components will be called as well.
cpacsPath must be filled
:Author: Jonas Jepsen
:param CPACSObj: the CPACS object holding the data for export
'''
# self.LoD.setValue(1) # level of detail [0,1]
if self.location.getValue():
xRoot = self.xRoot.getValue()
zRoot = self.zRoot.getValue()
else:
vtp_span = self.aircraft.vtp.span.getValue()
vtp_phiLE = (self.aircraft.vtp.phiLE.getValue())*pi/180.
xRoot = tan(vtp_phiLE)*vtp_span
try:
xRoot = xRoot.real
except:
pass
zRoot = vtp_span
createHTP(CPACSObj, self.id, xRoot, zRoot, self.airfoilr.tc.getValue(), self.airfoilt.tc.getValue(), self.cRoot.getValue(),
self.cTip.getValue(), self.span.getValue(), self.phiLE.getValue(), self.dihedral.getValue(),
self.LoD.getValue(), self.location.getValue())
super(wing, self).cpacsExport(CPACSObj)
def cpacsExport(self, CPACSObj):
'''
this methods exports all parameters nested in the component. Nested Components will be called as well.
cpacsPath must be filled
:Author: Jonas Jepsen
:param CPACSObj: the CPACS object holding the data for export
'''
xRoot = self.xRoot.getValue()
zRoot = self.zRoot.getValue()
createHTP(CPACSObj, self.id, xRoot, zRoot, self.airfoilr.tc.getValue(), self.airfoilt.tc.getValue(), self.cRoot.getValue(),
self.cTip.getValue(), self.span.getValue(), self.phiLE.getValue(), self.dihedral.getValue(),
self.LoD.getValue(), self.location.getValue())
super(wing, self).cpacsExport(CPACSObj)
