def createFuselageProfile(CPACSObj, profile='Circle' ):
'''
@author: Jonas Jepsen
'''
# get airfoil holding object
cpacsPath = '/cpacs/vehicles/profiles/fuselageProfiles/fuselageProfile[%s]'% profile
myProfile = getObjfromXpath(CPACSObj,cpacsPath)
pointList = myProfile.get_pointList()
if pointList is None:
#print "Airfoil 'Circle' not found -> will be created."
xVector, yVector, zVector = createCircleList()
# create pointList
pointList = pointListXYZVectorType()
x = stringVectorBaseType(mapType='vector',valueOf_=';'.join(xVector))
y = stringVectorBaseType(mapType='vector',valueOf_=';'.join(yVector))
z = stringVectorBaseType(mapType='vector',valueOf_=';'.join(zVector))
pointList.set_x(x)
pointList.set_y(y)
pointList.set_z(z)
myProfile.set_pointList(pointList)
myProfile.set_name(stringBaseType(valueOf_="Circle Profile"))
myProfile.set_description(stringBaseType(valueOf_="Profile generated automatically by VAMPzero cpacs-export" ))
def createFuselageProfile(CPACSObj, profile='Circle'):
'''
@author: Jonas Jepsen
'''
# get airfoil holding object
cpacsPath = '/cpacs/vehicles/profiles/fuselageProfiles/fuselageProfile[%s]' % profile
myProfile = getObjfromXpath(CPACSObj, cpacsPath)
pointList = myProfile.get_pointList()
if pointList is None:
#print "Airfoil 'Circle' not found -> will be created."
xVector, yVector, zVector = createCircleList()
# create pointList
pointList = pointListXYZVectorType()
x = stringVectorBaseType(None, None, None, 'vector', ';'.join(xVector))
y = stringVectorBaseType(None, None, None, 'vector', ';'.join(yVector))
z = stringVectorBaseType(None, None, None, 'vector', ';'.join(zVector))
pointList.set_x(x)
pointList.set_y(y)
pointList.set_z(z)
myProfile.set_pointList(pointList)
myProfile.set_name(stringBaseType(None, None, None, "Circle Profile"))
myProfile.set_description(
stringBaseType(
None, None, None,
"Profile generated automatically by VAMPzero cpacs-export"))
def cpacsExport(self, CPACSObj):
'''
This method overwrites the cpacsExport method of parameter.
This method will create the certification cases for CPACS
'''
def createPointList(nparray):
'''
create a point list for each cog location
This method is currently without use, as long as there is no update to CPACS 2.2.1
'''
myPointList = pointListType()
zero = doubleBaseType(valueOf_='0.')
for item in nparray.tolist():
newPoint = pointType(x=doubleBaseType(valueOf_=str(item)),y=zero, z=zero)
myPointList.add_point(newPoint)
return myPointList
def createVectorPointList(nparray):
'''
create a point list for each cog location
'''
myPointList = pointListType()
x = '; '.join(str(x) for x in nparray.tolist())
zeros = np.zeros(nparray.shape)
y = '; '.join(str(y) for y in zeros.tolist())
newPoint = pointType(x=doubleBaseType(valueOf_=str(x)),y=doubleBaseType(valueOf_=y), z=doubleBaseType(valueOf_=y))
myPointList.add_point(newPoint)
return myPointList
cpacsPath = '/cpacs/vehicles/aircraft/model/analyses/weightAndBalance/certificationCases'
myCertificationCases = getObjfromXpath(CPACSObj, cpacsPath)
# create mass Vector
massVector = stringVectorBaseType(valueOf_='; '.join(str(mass) for mass in self.m_TOW_fuel_pay.tolist()))
# create forward case, create backward case
forwardPoints = createVectorPointList(self.posCoGMIN_fuel_pay0)
rearwardPoints = createVectorPointList(self.posCoGMAX_fuel_pay0)
forwardCertificationCase = weightAndBalanceCaseType(uID="cc_forwardLocations", coG=forwardPoints, mass=massVector)
rearwardCertificationCase = weightAndBalanceCaseType(uID="cc_rearwardLocations", coG=rearwardPoints, mass=massVector)
myCertificationCases.add_certificationCase(forwardCertificationCase)
myCertificationCases.add_certificationCase(rearwardCertificationCase)
def createWingAirfoil(CPACSObj):
# get airfoil holding object
cpacsPath = '/cpacs/vehicles/profiles/wingAirfoils/wingAirfoil[NACA0009]'
myAirfoil = getObjfromXpath(CPACSObj, cpacsPath)
pointList = myAirfoil.get_pointList()
if pointList is None:
# print "Airfoil 'NACA0009' not found -> will be created."
# create pointList
pointList = pointListXYZVectorType()
xVector = []
yVector = []
zVector = []
for x, y in NACA0009[::-1]:
xVector.append(str(x))
yVector.append(str(0.0))
zVector.append(str(y))
x = stringVectorBaseType(mapType='vector',valueOf_=';'.join(xVector))
y = stringVectorBaseType(mapType='vector',valueOf_=';'.join(yVector))
z = stringVectorBaseType(mapType='vector',valueOf_=';'.join(zVector))
pointList.set_x(x)
pointList.set_y(y)
pointList.set_z(z)
myAirfoil.set_pointList(pointList)
myAirfoil.set_name(stringBaseType(valueOf_="NACA0009 Airfoil"))
myAirfoil.set_description(stringBaseType(valueOf_="Profile generated automatically by VAMPzero cpacs-export"))
# get airfoil holding object
cpacsPath = '/cpacs/vehicles/profiles/wingAirfoils/wingAirfoil[NACA653218]'
myAirfoil = getObjfromXpath(CPACSObj, cpacsPath)
pointList = myAirfoil.get_pointList()
if pointList is None:
# print "Airfoil 'NACA0000' not found -> will be created."
# create pointList
pointList = pointListXYZVectorType()
xVector = []
yVector = []
zVector = []
for x, y in NACA653218[::-1]:
xVector.append(str(x))
yVector.append(str(0.0))
zVector.append(str(y))
x = stringVectorBaseType(mapType='vector',valueOf_=';'.join(xVector))
y = stringVectorBaseType(mapType='vector',valueOf_=';'.join(yVector))
z = stringVectorBaseType(mapType='vector',valueOf_=';'.join(zVector))
pointList.set_x(x)
pointList.set_y(y)
pointList.set_z(z)
myAirfoil.set_pointList(pointList)
myAirfoil.set_name(stringBaseType(valueOf_="NACA653218 Airfoil"))
myAirfoil.set_description(stringBaseType(valueOf_="Profile generated automatically by VAMPzero cpacs-export"))
def createWingAirfoil(CPACSObj):
# get airfoil holding object
cpacsPath = '/cpacs/vehicles/profiles/wingAirfoils/wingAirfoil[NACA0009]'
myAirfoil = getObjfromXpath(CPACSObj, cpacsPath)
pointList = myAirfoil.get_pointList()
if pointList is None:
# print "Airfoil 'NACA0009' not found -> will be created."
# create pointList
pointList = pointListXYZVectorType()
xVector = []
yVector = []
zVector = []
for x, y in NACA0009:
xVector.append(str(x))
yVector.append(str(0.0))
zVector.append(str(y))
x = stringVectorBaseType(None, None, None, 'vector', ';'.join(xVector))
y = stringVectorBaseType(None, None, None, 'vector', ';'.join(yVector))
z = stringVectorBaseType(None, None, None, 'vector', ';'.join(zVector))
pointList.set_x(x)
pointList.set_y(y)
pointList.set_z(z)
myAirfoil.set_pointList(pointList)
myAirfoil.set_name(stringBaseType(None, None, None,
"NACA0009 Airfoil"))
myAirfoil.set_description(
stringBaseType(
None, None, None,
"Profile generated automatically by VAMPzero cpacs-export"))
# get airfoil holding object
cpacsPath = '/cpacs/vehicles/profiles/wingAirfoils/wingAirfoil[NACA653218]'
myAirfoil = getObjfromXpath(CPACSObj, cpacsPath)
pointList = myAirfoil.get_pointList()
if pointList is None:
# print "Airfoil 'NACA0000' not found -> will be created."
# create pointList
pointList = pointListXYZVectorType()
xVector = []
yVector = []
zVector = []
for x, y in NACA653218:
xVector.append(str(x))
yVector.append(str(0.0))
zVector.append(str(y))
x = stringVectorBaseType(None, None, None, 'vector', ';'.join(xVector))
y = stringVectorBaseType(None, None, None, 'vector', ';'.join(yVector))
z = stringVectorBaseType(None, None, None, 'vector', ';'.join(zVector))
pointList.set_x(x)
pointList.set_y(y)
pointList.set_z(z)
myAirfoil.set_pointList(pointList)
myAirfoil.set_name(
stringBaseType(None, None, None, "NACA653218 Airfoil"))
myAirfoil.set_description(
stringBaseType(
None, None, None,
"Profile generated automatically by VAMPzero cpacs-export"))