def _process_fuse(compound, divide_closed, name):
# For VSP fuselages, the longitudinal direction is u, and the
# circumferential direction is v.
# Build the solid.
solid, invalid = _build_solid(compound, divide_closed)
if not solid:
return None, invalid
fuselage = Body(solid, name)
faces = compound.faces
if len(faces) == 1:
vsp_surf = faces[0].surface
fuselage.metadata.set('vsp surface', vsp_surf)
return fuselage, invalid
def save_bodies(self, fn):
"""
Save the Body instances.
:param str fn: The filename. The extension will be ".xbf" and appended
if not provided.
:return: *True* if saved, *False* otherwise.
:rtype: bool
.. note::
This method only saves the label, shape, and color of the Body.
User-defined metadata is currently not saved.
"""
bodies = list(self.bodies.values())
return Body.save_bodies(fn, *bodies)
def _process_wing(compound, divide_closed, bspline_restrict, tol, reloft,
name):
# Note that for VSP wings, the spanwise direction is u and the chord
# direction is v, where v=0 is the TE and follows the lower surface fwd to
# the LE, and then aft along the upper surface to the TE.
# Process based on number of faces in compound assuming split/no split
# option was used.
faces = compound.faces
vsp_surf = None
if len(faces) == 1:
solid, invalid = _process_unsplit_wing(compound, divide_closed, reloft,
tol)
vsp_surf = faces[0].surface
else:
solid, invalid = _build_solid(compound, divide_closed)
if not solid:
return None
if bspline_restrict:
solid = _bspline_restrict(solid, tol)
wing = Body(solid, name)
if vsp_surf:
wing.metadata.set('vsp surface', vsp_surf)
upr_srf = vsp_surf.copy()
v_le = vsp_surf.local_to_global_param('v', 0.5)
upr_srf.segment(vsp_surf.u1, vsp_surf.u2, v_le, vsp_surf.v2)
wing.metadata.set('upper surface', upr_srf)
lwr_srf = vsp_surf.copy()
lwr_srf.segment(vsp_surf.u1, vsp_surf.u2, vsp_surf.v1, v_le)
wing.metadata.set('lower surface', lwr_srf)
return wing, invalid
def import_step(self, fn):
"""
Import a STEP file generated by the OpenVSP version that has been
modified to include metadata.
:param str fn: The full path to the file.
:return: None.
"""
# Store data as dictionaries.
bodies = {}
indx = 0
# Dictionaries to attach wing reference surfaces to wing bodies using
# reference surface ID as the key.
wing_bodies = {}
ref_surfs = {}
# Data structures for fuselage reference surfaces
fuselage_bodies = {}
href_surfs = {}
vref_surfs = {}
# Read STEP file
step_reader = StepRead(fn)
master_shape = step_reader.shape
# Iterate over master shape to find compounds for geometric sets. These
# sets contain the metadata and the surfaces that make up the
# component.
for compound in master_shape.shape_iter:
# Get the metadata
name = step_reader.name_from_shape(compound)
# Unnamed body
if not name:
indx += 1
comp_name = '.'.join(['Body', str(indx)])
msg = ' '.join(['---Processing OpenVSP component:', comp_name])
logger.info(msg)
solid, invalid = _build_solid(compound, self._divide)
self._invalid += invalid
if solid is not None:
body = Body(solid, comp_name)
bodies[comp_name] = body
continue
metadata = json.loads(name)
# Process reference surfaces and continue
key = 'm_SurfType'
if key in metadata and metadata[key] == 99:
# Get surface
sref = ImportVSP.process_sref(compound)
# Get Sref ID
sref_id = metadata['ID']
ref_surfs[sref_id] = sref
continue
elif key in metadata and metadata[key] == 100:
# Fuselage horizontal sref
f = compound.faces[0]
sref = f.surface
sref.set_udomain(-1., 1.)
sref.set_vdomain(0., 1.)
sref.object.ExchangeUV()
sref.object.UReverse()
sref_id = metadata['ID']
href_surfs[sref_id] = sref
continue
elif key in metadata and metadata[key] == 101:
f = compound.faces[0]
sref = f.surface
sref.set_udomain(-1., 1.)
sref.set_vdomain(0., 1.)
sref.object.ExchangeUV()
sref.object.UReverse()
sref_id = metadata['ID']
vref_surfs[sref_id] = sref
continue
comp_name = metadata['m_Name']
if comp_name in bodies:
indx += 1
comp_name = '.'.join([comp_name, str(indx)])
# Process component.
msg = ' '.join(['---Processing OpenVSP component:', comp_name])
logger.info(msg)
# Wing
if metadata['m_Type'] == 5 and metadata['m_SurfType'] != 99:
wing, invalid = _process_wing(compound, self._divide,
self._restrict, self._tol,
self._reloft, comp_name)
self._invalid += invalid
if wing is not None:
bodies[comp_name] = wing
sref_id = metadata['Sref ID']
wing_bodies[sref_id] = wing
# Fuselage
elif metadata['m_Type'] in [4, 9]:
fuse, invalid = _process_fuse(compound, self._divide,
comp_name)
self._invalid += invalid
if fuse is not None:
bodies[comp_name] = fuse
sref_id = metadata['Sref ID']
fuselage_bodies[sref_id] = fuse
# Unknown
else:
solid, invalid = _build_solid(compound, self._divide)
self._invalid += invalid
if solid:
body = Body(solid, comp_name)
bodies[comp_name] = body
# Attach wing reference surfaces to the bodies.
for sref_id in wing_bodies:
if sref_id not in ref_surfs:
continue
wing = wing_bodies[sref_id]
sref = ref_surfs[sref_id]
wing.set_sref(sref)
# Attach fuselage reference surfaces to the bodies.
for sref_id in fuselage_bodies:
if sref_id in href_surfs:
fuselage = fuselage_bodies[sref_id]
sref = href_surfs[sref_id]
fuselage.metadata.set('hsref', sref)
if sref_id in vref_surfs:
fuselage = fuselage_bodies[sref_id]
sref = vref_surfs[sref_id]
fuselage.metadata.set('vsref', sref)
# Update
self._bodies.update(bodies)