def __init__(self, aircraft):
'''
initializes fuselage object
mostly used for documentation
establishes link to the aircraft class
@Method: Component Constructor
'''
component.__init__(self)
self.id = 'fuselage'
self.aircraft = aircraft
self.level = 2
#Mass
self.mFuselage = mFuselage()
self.mFurn = mFurn(
cpacsPath='/cpacs/vehicles/aircraft/model/analyses/massBreakdown/mOEM/mEM/mFurnishing/massDescription/mass')
self.mStructure = mStructure(
cpacsPath='/cpacs/vehicles/aircraft/model/analyses/massBreakdown/mOEM/mEM/mStructure/mFuselagesStructure/mFuselageStructure/massDescription/mass')
#CoG
self.posCoG = posCoG(
cpacsPath='/cpacs/vehicles/aircraft/model/analyses/massBreakdown/mOEM/mEM/mStructure/mFuselagesStructure/mFuselageStructure/massDescription/location/x')
#Geometry
self.xRoot = xRoot()# the fuselages origin
self.dfus = dfus()
self.lfus = lfus()#cpacsPath='/cpacs/toolspecific/joeFuMo/lfuselage')
self.lcabin = lcabin()#cpacsPath='/cpacs/toolspecific/joeFuMo/deck/length')
self.lcockpit = lcockpit()
self.lnose = lnose()#cpacsPath='/cpacs/toolspecific/joeFuMo/lnose')
self.ltail = ltail()#cpacsPath='/cpacs/toolspecific/joeFuMo/ltail')
self.loverlay = loverlay()#cpacsPath='/cpacs/toolspecific/joeFuMo/loverlay')
self.wetArea = wetArea()
self.LoD = LoD()
#Cabin
self.nRow = nRow()
self.nPaxR = nPaxR()
self.nAisle = nAisle()
self.nClasses = nClasses()
self.refLayout = refLayout()#cpacsPath='/cpacs/toolspecific/joeFuMo/deck/refLayout',)
self.refAbreast = refAbreast()#cpacsPath='/cpacs/toolspecific/joeFuMo/deck/refAbreast',)
self.cargoDeck = cargoDeck()#cpacsPath='/cpacs/toolspecific/joeFuMo/cargoDeck')
self.paxDensity = paxDensity()
self.dcabin = dcabin()
self.hcabin = hcabin()
self.vcabin = vcabin()
self.yFloor = yFloor()
self.zFloor = zFloor()
#Aerodynamics
self.formFactor = formFactor()
self.reynoldsNr = reynoldsNr()
self.cfLAM = cfLAM()
self.cfTURB = cfTURB()
self.cD0c = cD0c()
self.dragArea = dragArea()
self.nLam = nLam()
class fuselage(component):
'''
fuselage Class
'''
def __init__(self, aircraft):
'''
initializes fuselage object
mostly used for documentation
establishes link to the aircraft class
@Method: Component Constructor
'''
component.__init__(self)
self.id = 'fuselage'
self.aircraft = aircraft
self.level = 2
#Mass
self.mFuselage = mFuselage()
self.mFurn = mFurn(
cpacsPath='/cpacs/vehicles/aircraft/model/analyses/massBreakdown/mOEM/mEM/mFurnishing/massDescription/mass')
self.mStructure = mStructure(
cpacsPath='/cpacs/vehicles/aircraft/model/analyses/massBreakdown/mOEM/mEM/mStructure/mFuselagesStructure/mFuselageStructure/massDescription/mass')
#CoG
self.posCoG = posCoG(
cpacsPath='/cpacs/vehicles/aircraft/model/analyses/massBreakdown/mOEM/mEM/mStructure/mFuselagesStructure/mFuselageStructure/massDescription/location/x')
#Geometry
self.xRoot = xRoot()# the fuselages origin
self.dfus = dfus()
self.lfus = lfus()#cpacsPath='/cpacs/toolspecific/joeFuMo/lfuselage')
self.lcabin = lcabin()#cpacsPath='/cpacs/toolspecific/joeFuMo/deck/length')
self.lcockpit = lcockpit()
self.lnose = lnose()#cpacsPath='/cpacs/toolspecific/joeFuMo/lnose')
self.ltail = ltail()#cpacsPath='/cpacs/toolspecific/joeFuMo/ltail')
self.loverlay = loverlay()#cpacsPath='/cpacs/toolspecific/joeFuMo/loverlay')
self.wetArea = wetArea()
self.LoD = LoD()
#Cabin
self.nRow = nRow()
self.nPaxR = nPaxR()
self.nAisle = nAisle()
self.nClasses = nClasses()
self.refLayout = refLayout()#cpacsPath='/cpacs/toolspecific/joeFuMo/deck/refLayout',)
self.refAbreast = refAbreast()#cpacsPath='/cpacs/toolspecific/joeFuMo/deck/refAbreast',)
self.cargoDeck = cargoDeck()#cpacsPath='/cpacs/toolspecific/joeFuMo/cargoDeck')
self.paxDensity = paxDensity()
self.dcabin = dcabin()
self.hcabin = hcabin()
self.vcabin = vcabin()
self.yFloor = yFloor()
self.zFloor = zFloor()
#Aerodynamics
self.formFactor = formFactor()
self.reynoldsNr = reynoldsNr()
self.cfLAM = cfLAM()
self.cfTURB = cfTURB()
self.cD0c = cD0c()
self.dragArea = dragArea()
self.nLam = nLam()
###################################################################################################
##Export to CPACS
###################################################################################################
def cpacsExport(self, CPACSObj):
'''
this methods exports all parameters nested in the component. Nested Components will be called as well.
cpacsPath must be filled
'''
# level of detail
self.log.debug("lfus,lcabin,lcockpit,lnose,ltail,loverlay: %s, %s, %s, %s, %s, %s" % (
self.lfus.getValue(), self.lcabin.getValue(), self.lcockpit.getValue(), self.lnose.getValue(),
self.ltail.getValue(), self.loverlay.getValue()))
createFuselageProfile(CPACSObj, 'Circle')
createFuselage(CPACSObj, self.id, self.dfus.getValue(), self.lnose.getValue(),
self.lfus.getValue() - self.ltail.getValue() - self.lnose.getValue(), self.ltail.getValue(),
self.LoD.getValue())
super(fuselage, self).cpacsExport(CPACSObj)
