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
'''
if self.active.getValue():
createWing(CPACSObj, id=self.id, zeroWing=self, LoD=WING_LOD.STRUT)
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
"""
if self.active.getValue():
createWing(CPACSObj, id=self.id, zeroWing=self, LoD=WING_LOD.STRUT)
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
'''
if self.aircraft.strut.active.getValue():
self.LoD.setValueCalc(WING_LOD.SBW)
try:
etaKink = self.etaKink.getValue()
etaEngine = self.aircraft.engine.yEngine.getValue() / self.span.getValue() * 2.
createWingAirfoil(CPACSObj)
createWing(CPACSObj, id=self.id, zeroWing=self, LoD=self.LoD.getValue())
except ZeroDivisionError, e:
self.log.warning('VAMPzero EXPORT: WING could not be created due to "%s"!', e)
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
'''
if self.aircraft.strut.active.getValue():
self.LoD.setValueFix(WING_LOD.SBW)
try:
etaKink = self.etaKink.getValue()
etaEngine = self.aircraft.engine.yEngine.getValue(
) / self.span.getValue() * 2.
createWingAirfoil(CPACSObj)
createWing(CPACSObj,
id=self.id,
zeroWing=self,
LoD=self.LoD.getValue())
except ZeroDivisionError, e:
self.log.warning(
'VAMPzero EXPORT: WING could not be created due to "%s"!', e)