def test_A(self):
cid0 = CORD2R()
Lx = 2.
Ly = 0.
Lz = 3.
Fy = 1.
origin = array([-Lx, 0., -Lz])
z_axis = origin + array([0., 0., 1.])
xz_plane = origin + array([1., 0., 1.])
rid = 0
data = [1, rid] + list(origin) + list(z_axis) + list(xz_plane)
Fxyz = [0., -Fy, 0.]
Mxyz = [0., 0., 0.]
cid_new = CORD2R(data=data)
model = None
Fxyz_local, Mxyz_local = TransformLoadWRT(Fxyz, Mxyz, cid0, cid_new,
model, is_cid_int=False)
r = array([Lx, Ly, Lz])
F = array([0., -Fy, 0.])
M = cross(r, F)
self.assertTrue(array_equal(Fxyz_local, F)), "expected=%s actual=%s" % (F, Fxyz_local)
self.assertTrue(array_equal(Mxyz_local, cross(r, F))), "expected=%s actual=%s" % (M, Mxyz_local)
def test_coord_xform_b(self):
origin = array([0., 0., 0.])
zaxis = array([0., 0., 1.])
xzplane = array([1., 0., 0.])
cid0 = CORD2R(cid=0, rid=0, origin=origin, zaxis=zaxis, xzplane=xzplane)
Lx = 2.
Ly = 3.
Lz = 5.
Fy = 1.5
origin = array([-Lx, -Ly, -Lz])
z_axis = origin + array([0., 0., 1.])
xz_plane = origin + array([1., 0., 1.])
rid = 0
data = [1, rid] + list(origin) + list(z_axis) + list(xz_plane)
fxyz = [0., -Fy, 0.]
mxyz = [0., 0., 0.]
cid_new = CORD2R.add_op2_data(data=data)
model = None
fxyz_local, mxyz_local = TransformLoadWRT(fxyz, mxyz, cid0, cid_new,
model, is_cid_int=False)
r = array([Lx, Ly, Lz])
F = array([0., -Fy, 0.])
M = cross(r, F)
self.assertTrue(array_equal(fxyz_local, F), 'expected=%s actual=%s' % (F, fxyz_local))
self.assertTrue(array_equal(mxyz_local, M), 'expected=%s actual=%s' % (M, mxyz_local))
def test_caero3_1(self):
"""checks the CAERO3/PAERO3"""
eid = 100
pid = 200
cp = 4
list_w = 5
list_c1 = 6
list_c2 = 7
p1 = [0., 0., 0.]
x12 = 10.
p4 = [5., 10., 0.]
x43 = 3.
nbox = 10
ncontrol_surfaces = 0
x = None
y = None
log = SimpleLogger(level='warning')
model = BDF(log=log)
coord = CORD2R.add_card(BDFCard(['CORD2R', cp, 0,
0., 0., 0.,
0., 0., 1.,
1., 0., 0.]))
coord = CORD2R(cp, rid=0, origin=None, zaxis=None, xzplane=None,
comment='')
coord.validate()
model.coords[cp] = coord
paero = PAERO3(pid, nbox, ncontrol_surfaces, x, y)
model.paeros[pid] = paero
card = ['CAERO3', 2000, 20001, 0, 22, 33, None, None, None,
1.0, 0.0, 0., 100., 17., 130., 0., 100.]
bdf_card = BDFCard(card, has_none=True)
caero3a = CAERO3.add_card(bdf_card, comment='msg')
caero3a.validate()
caero3a.write_card()
caero3a.raw_fields()
caero3b = CAERO3(eid, pid, cp, list_w, list_c1, list_c2, p1, x12, p4,
x43, comment='caero3')
model.caeros[pid] = caero3b
caero3b.write_card()
caero3b.cross_reference(model)
caero3b.write_card()
caero3a.raw_fields()
caero3b.uncross_reference()
caero3b.write_card()
caero3a.raw_fields()
def test_cut_shell_model_face_1(self):
"""
tests:
- cut_edge_model_by_coord
- cut_face_model_by_coord
"""
tol = 2.
coord = CORD2R(1, rid=0, origin=[0.5, 0., 0.], zaxis=[0.5, 0., 1], xzplane=[1.5, 0., 0.],
comment='')
model, nodal_result = _cut_shell_model_quads()
#-------------------------------------------------------------------------
# triangles
split_to_trias(model)
model.coords[1] = coord
model.write_bdf('tris.bdf')
#print('----------------------------')
title = 'result'
p1 = None
p2 = None
zaxis = None
#print(nodal_result)
with self.assertRaises(TypeError):
cut_and_plot_model(title, p1, p2, zaxis,
model, coord, nodal_result, model.log, tol,
plane_atol=1e-5,
csv_filename=None,
invert_yaxis=False,
cut_type='face', plot=IS_MATPLOTLIB, show=False)
os.remove('tris.bdf')
def test_cord2c_01(self):
lines = [
'CORD2C* 3 0 0. 0.',
'* 0. 0. 0. 1.*',
'* 1. 0. 1.'
]
model = BDF(debug=False)
card = model.process_card(lines)
card = BDFCard(card)
card = CORD2C(card)
model.add_coord(card)
lines = [
'CORD2R 4 3 10. 0. 5. 10. 90. 5.',
' 10. 0. 6.'
]
card = model.process_card(lines)
card = BDFCard(card)
card = CORD2R(card)
model.add_coord(card)
model.cross_reference()
cord2r = model.Coord(3)
self.assertEquals(cord2r.Cid(), 3)
self.assertEquals(cord2r.Rid(), 0)
cord2r = model.Coord(4)
self.assertEquals(cord2r.Cid(), 4)
self.assertEquals(cord2r.Rid(), 3)
self.assertTrue(allclose(cord2r.i, array([0., 0., 1.])))
delta = cord2r.j - array([1., 1., 0.]) / 2**0.5
self.assertTrue(allclose(cord2r.j, array([1., 1., 0.]) / 2**0.5), str(delta))
delta = cord2r.k - array([-1., 1., 0.]) / 2**0.5
self.assertTrue(allclose(cord2r.k, array([-1., 1., 0.]) / 2**0.5), str(delta))
def test_B(self):
origin = array([0., 0., 0.])
zaxis = array([0., 0., 1.])
xzplane = array([1., 0., 0.])
cid0 = CORD2R(cid=0, rid=0, origin=origin, zaxis=zaxis, xzplane=xzplane)
Lx = 2.
Ly = 3.
Lz = 5.
Fy = 1.5
origin = array([-Lx, -Ly, -Lz])
z_axis = origin + array([0., 0., 1.])
xz_plane = origin + array([1., 0., 1.])
rid = 0
data = [1, rid] + list(origin) + list(z_axis) + list(xz_plane)
Fxyz = [0., -Fy, 0.]
Mxyz = [0., 0., 0.]
cid_new = CORD2R.add_op2_data(data=data)
model = None
Fxyz_local, Mxyz_local = TransformLoadWRT(Fxyz, Mxyz, cid0, cid_new,
model, is_cid_int=False)
r = array([Lx, Ly, Lz])
F = array([0., -Fy, 0.])
M = cross(r, F)
self.assertTrue(array_equal(Fxyz_local, F)), "expected=%s actual=%s" % (F, Fxyz_local)
self.assertTrue(array_equal(Mxyz_local, cross(r, F))), "expected=%s actual=%s" % (M, Mxyz_local)
def plot_shear_moment_torque(model,
gpforce,
coord: CORD2R,
idir: int = 0,
itime: int = 0,
nplanes: int = 11,
show: bool = True):
nids, nid_cd, xyz_cid0, icd_transform, eids, element_centroids_cid0 = smt_setup(
model)
element_centroids_cid = coord.transform_node_to_local_array(
element_centroids_cid0)
x = element_centroids_cid[idir]
xmin = x.min()
xmax = x.max()
dx = xmax - xmin
assert abs(dx) > 0., f'dx={dx} xmin={xmin} xmax={xmax}'
stations = np.linspace(0., dx, num=nplanes, endpoint=True)
force_sum, moment_sum = gpforce.shear_moment_diagram(
xyz_cid0,
eids,
nids,
icd_transform,
element_centroids_cid0,
model.coords,
nid_cd,
stations,
coord,
idir=idir,
itime=itime,
debug=False,
log=model.log)
plot_smt(stations, force_sum, moment_sum, show=show)
def test_cut_plate(self):
"""mode 10 is a sine wave"""
log = SimpleLogger(level='warning', encoding='utf-8', log_func=None)
bdf_filename = os.path.join(MODEL_PATH, 'plate_py', 'plate_py.dat')
op2_filename = os.path.join(MODEL_PATH, 'plate_py', 'plate_py.op2')
model = read_bdf(bdf_filename, log=log)
op2_model = read_op2_geom(op2_filename, log=log)
title = 'Mode 10 Eigenvector'
p1 = None
p2 = None
zaxis = None
coord = CORD2R(1,
rid=0,
origin=[0., 0., 0.],
zaxis=[0., 0., 1],
xzplane=[1., 0., 0.],
comment='')
model.coords[1] = coord
ytol = 2.
# real
nodal_result = op2_model.eigenvectors[1].data[9, :, 2]
cut_and_plot_model(title,
p1,
p2,
zaxis,
model,
coord,
nodal_result,
model.log,
ytol,
plane_atol=1e-5,
csv_filename='real_result.csv',
invert_yaxis=False,
cut_type='edge',
plot=IS_MATPLOTLIB,
show=False)
# complex
nodal_result2 = np.asarray(nodal_result, dtype='complex64')
nodal_result2.imag = -nodal_result.real
cut_and_plot_model(title,
p1,
p2,
zaxis,
model,
coord,
nodal_result2,
model.log,
ytol,
plane_atol=1e-5,
csv_filename='complex_result.csv',
invert_yaxis=True,
cut_type='edge',
plot=IS_MATPLOTLIB,
show=False)
os.remove('real_result.csv')
os.remove('complex_result.csv')
def test_cut_plate_eids(self):
"""recover element ids"""
log = SimpleLogger(level='warning', encoding='utf-8', log_func=None)
bdf_filename = os.path.join(MODEL_PATH, 'plate_py', 'plate_py.dat')
model = read_bdf(bdf_filename, log=log)
nnodes = len(model.nodes)
nodal_result = np.ones(nnodes)
coord = CORD2R(1, rid=0, origin=[0., 0., 0.], zaxis=[0., 0., 1], xzplane=[1., 0., 0.],
comment='')
model.coords[1] = coord
ytol = 2.
unique_geometry_array, unique_results_array, unused_rods = cut_face_model_by_coord(
bdf_filename, coord, ytol,
nodal_result, plane_atol=1e-5, skip_cleanup=True,
csv_filename='cut_face.csv')
#print(unique_geometry_array)
#print(unique_results_array)
unique_geometry_array = np.array(unique_geometry_array)
unique_results_array = np.array(unique_results_array)
assert unique_geometry_array.shape == (1, 40, 4), unique_geometry_array.shape
assert unique_results_array.shape == (1, 40, 7), unique_results_array.shape
unique_geometry_array = unique_geometry_array[0, :, :]
unique_results_array = unique_results_array[0, :, :]
assert unique_geometry_array.shape == (40, 4), unique_geometry_array.shape
assert unique_results_array.shape == (40, 7), unique_results_array.shape
def test_cord2c_01(self):
lines = [
'CORD2C* 3 0 0. 0.',
'* 0. 0. 0. 1.*',
'* 1. 0. 1.'
]
model = BDF(debug=False)
card = model.process_card(lines)
cardi = BDFCard(card)
coord = CORD2C.add_card(cardi)
model.add_coord(coord)
lines = [
'CORD2R 4 3 10. 0. 5. 10. 90. 5.',
' 10. 0. 6.'
]
card = model.process_card(lines)
cardi = BDFCard(card)
coord = CORD2R.add_card(cardi)
model.add_coord(coord)
model.cross_reference()
cord2r = model.Coord(3)
self.assertEqual(cord2r.Cid(), 3)
self.assertEqual(cord2r.Rid(), 0)
cord2r = model.Coord(4)
self.assertEqual(cord2r.Cid(), 4)
self.assertEqual(cord2r.Rid(), 3)
self.assertTrue(allclose(cord2r.i, array([0., 0., 1.])))
delta = cord2r.j - array([1., 1., 0.]) / 2**0.5
self.assertTrue(allclose(cord2r.j, array([1., 1., 0.]) / 2**0.5), str(delta))
delta = cord2r.k - array([-1., 1., 0.]) / 2**0.5
self.assertTrue(allclose(cord2r.k, array([-1., 1., 0.]) / 2**0.5), str(delta))
def get_coords_crm(ncuts=2000): # pragma: no cover
dys = []
coords = []
for i in range(ncuts):
dy = 4. * i + 1. # CRM
coord = CORD2R(1, rid=0, origin=[0., dy, 0.], zaxis=[0., dy, 1], xzplane=[1., dy, 0.])
dys.append(dy)
coords.append(coord)
return dys, coords
def get_coords_bwb(ncuts=2000):
dys = []
coords = []
for i in range(ncuts):
dy = 100. * i + 1. # bwb
coord = CORD2R(1, rid=0, origin=[0., dy, 0.], zaxis=[0., dy, 1], xzplane=[1., dy, 0.])
dys.append(dy)
coords.append(coord)
return dys, coords
def test_caero3_1(self):
"""checks the CAERO3/PAERO3"""
eid = 100
pid = 200
cp = 4
list_w = 5
list_c1 = 6
list_c2 = 7
p1 = [0., 0., 0.]
x12 = 10.
p4 = [5., 10., 0.]
x43 = 3.
nbox = 10
ncontrol_surfaces = 0
x = None
y = None
log = SimpleLogger(level='warning')
model = BDF(log=log)
coord = CORD2R.add_card(BDFCard(['CORD2R', cp, 0,
0., 0., 0.,
0., 0., 1.,
1., 0., 0.]))
coord = CORD2R(cp, rid=0, origin=None, zaxis=None, xzplane=None,
comment='')
coord.validate()
model.coords[cp] = coord
paero = PAERO3(pid, nbox, ncontrol_surfaces, x, y)
model.paeros[pid] = paero
card = ['CAERO3', 2000, 20001, 0, 22, 33, None, None, None,
1.0, 0.0, 0., 100., 17., 130., 0., 100.]
bdf_card = BDFCard(card, has_none=True)
caero3a = CAERO3.add_card(bdf_card, comment='msg')
caero3a.validate()
caero3a.write_card()
caero3a.raw_fields()
caero3b = CAERO3(eid, pid, cp, list_w, list_c1, list_c2, p1, x12, p4,
x43, comment='caero3')
model.caeros[pid] = caero3b
caero3b.write_card()
caero3b.cross_reference(model)
caero3b.write_card()
caero3a.raw_fields()
caero3b.uncross_reference()
caero3b.write_card()
caero3a.raw_fields()
def test_coord_adding(self):
origin = [0., 0., 0.]
zaxis = [0., 0., 1.]
xzplane = [1., 0., 0.]
cid1 = CORD2R(cid=1, rid=0, origin=origin, zaxis=zaxis, xzplane=xzplane,
comment='cord2r')
xaxis = [1., 0., 0.]
yaxis = [0., 1., 0.]
zaxis = [0., 0., 1.]
xz_plane = [1., 0., 1.]
yz_plane = [0., 1., 1.]
xy_plane = [1., 1., 0.]
# x-axis
cid2 = CORD2R.add_axes(cid=2, rid=0, origin=origin, xaxis=xaxis, yaxis=None, zaxis=None,
xyplane=None, yzplane=None, xzplane=xz_plane)
cid3 = CORD2R.add_axes(cid=2, rid=0, origin=origin, xaxis=xaxis, yaxis=None, zaxis=None,
xyplane=xy_plane, yzplane=None, xzplane=None)
# y-axis
cid4 = CORD2R.add_axes(cid=4, rid=0, origin=origin, xaxis=None, yaxis=yaxis, zaxis=None,
xyplane=xy_plane, yzplane=None, xzplane=None)
cid5 = CORD2R.add_axes(cid=5, rid=0, origin=origin, xaxis=None, yaxis=yaxis, zaxis=None,
xyplane=None, yzplane=yz_plane, xzplane=None)
# z-axis
cid4 = CORD2R.add_axes(cid=4, rid=0, origin=origin, xaxis=None, yaxis=None, zaxis=zaxis,
xyplane=None, yzplane=None, xzplane=xz_plane)
cid5 = CORD2R.add_axes(cid=5, rid=0, origin=origin, xaxis=None, yaxis=None, zaxis=zaxis,
xyplane=None, yzplane=yz_plane, xzplane=None)
# ijk
cid6 = CORD2R.add_ijk(cid=6, rid=0, origin=origin, i=xaxis, j=yaxis, k=None)
cid7 = CORD2R.add_ijk(cid=7, rid=0, origin=origin, i=xaxis, j=None, k=zaxis)
cid8 = CORD2R.add_ijk(cid=8, rid=0, origin=origin, i=None, j=yaxis, k=zaxis)
def test_cut_shell_model_1(self):
"""
tests:
- cut_edge_model_by_coord
- cut_face_model_by_coord
"""
model, nodal_result = _cut_shell_model_quads()
coord = CORD2R(1,
rid=0,
origin=[0.5, 0., 0.],
zaxis=[0.5, 0., 1],
xzplane=[1.5, 0., 0.],
comment='')
model.coords[1] = coord
tol = 2.
#-------------------------------------------------------------------------
title = 'result'
p1 = None
p2 = None
zaxis = None
cut_and_plot_model(title,
p1,
p2,
zaxis,
model,
coord,
nodal_result,
model.log,
tol,
plane_atol=1e-5,
csv_filename=None,
invert_yaxis=False,
cut_type='edge',
plot=IS_MATPLOTLIB,
show=False)
#=========================================================================
out = cut_edge_model_by_coord(model,
coord,
tol,
nodal_result,
plane_atol=1e-5)
unused_local_points_array, unused_global_points_array, result_array = out
assert len(result_array) == 16, len(result_array)
unused_geometry_array, result_array, unused_rods = cut_face_model_by_coord(
model, coord, tol, nodal_result, plane_atol=1e-5)
result_array = np.array(result_array)
assert result_array.shape == (1, 8, 7), result_array.shape
os.remove('plane_edge.bdf')
os.remove('plane_face.bdf')
def test_cut_shell_model_1(self):
"""
tests:
- cut_edge_model_by_coord
- cut_face_model_by_coord
"""
model, nodal_result = _cut_shell_model_quads()
coord = CORD2R(1,
rid=0,
origin=[0.5, 0., 0.],
zaxis=[0.5, 0., 1],
xzplane=[1.5, 0., 0.],
comment='')
model.coords[1] = coord
tol = 2.
#-------------------------------------------------------------------------
title = 'result'
p1 = None
p2 = None
zaxis = None
cut_and_plot_model(title,
p1,
p2,
zaxis,
model,
coord,
nodal_result,
model.log,
tol,
plane_atol=1e-5,
csv_filename=None,
invert_yaxis=False,
cut_type='edge',
show=False)
#=========================================================================
local_points_array, global_points_array, result_array = cut_edge_model_by_coord(
model, coord, tol, nodal_result, plane_atol=1e-5)
assert len(result_array) == 16, len(result_array)
geometry_array, result_array = cut_face_model_by_coord(model,
coord,
tol,
nodal_result,
plane_atol=1e-5)
assert result_array is None, len(result_array) # no quad support
os.remove('plane_edge.bdf')
os.remove('plane_face.bdf')
def test_coord_adding(self):
origin = [0., 0., 0.]
zaxis = [0., 0., 1.]
xzplane = [1., 0., 0.]
cid1 =CORD2R(cid=1, rid=0, origin=origin, zaxis=zaxis, xzplane=xzplane,
comment='')
xaxis = [1., 0., 0.]
yaxis = [0., 1., 0.]
zaxis = [0., 0., 1.]
xz_plane = [1., 0., 1.]
yz_plane = [0., 1., 1.]
xy_plane = [1., 1., 0.]
# x-axis
cid2 = CORD2R.add_axes(cid=2, rid=0, origin=origin, xaxis=xaxis, yaxis=None, zaxis=None,
xyplane=None, yzplane=None, xzplane=xz_plane)
cid3 = CORD2R.add_axes(cid=2, rid=0, origin=origin, xaxis=xaxis, yaxis=None, zaxis=None,
xyplane=xy_plane, yzplane=None, xzplane=None)
# y-axis
cid4 = CORD2R.add_axes(cid=4, rid=0, origin=origin, xaxis=None, yaxis=yaxis, zaxis=None,
xyplane=xy_plane, yzplane=None, xzplane=None)
cid5 = CORD2R.add_axes(cid=5, rid=0, origin=origin, xaxis=None, yaxis=yaxis, zaxis=None,
xyplane=None, yzplane=yz_plane, xzplane=None)
# z-axis
cid4 = CORD2R.add_axes(cid=4, rid=0, origin=origin, xaxis=None, yaxis=None, zaxis=zaxis,
xyplane=None, yzplane=None, xzplane=xz_plane)
cid5 = CORD2R.add_axes(cid=5, rid=0, origin=origin, xaxis=None, yaxis=None, zaxis=zaxis,
xyplane=None, yzplane=yz_plane, xzplane=None)
# ijk
cid6 = CORD2R.add_ijk(cid=6, rid=0, origin=origin, i=xaxis, j=yaxis, k=None)
cid7 = CORD2R.add_ijk(cid=7, rid=0, origin=origin, i=xaxis, j=None, k=zaxis)
cid8 = CORD2R.add_ijk(cid=8, rid=0, origin=origin, i=None, j=yaxis, k=zaxis)
def test_cut_shell_model_2(self):
"""
tests:
- cut_edge_model_by_coord
- cut_face_model_by_coord
"""
tol = 2.
coord = CORD2R(1, rid=0, origin=[0.5, 0., 0.], zaxis=[0.5, 0., 1], xzplane=[1.5, 0., 0.],
comment='')
model, nodal_result = _cut_shell_model_quads()
#-------------------------------------------------------------------------
# triangles
split_to_trias(model)
model.coords[1] = coord
model.write_bdf('tris.bdf')
#print('----------------------------')
title = 'result'
p1 = None
p2 = None
zaxis = None
cut_and_plot_model(title, p1, p2, zaxis,
model, coord, nodal_result, model.log, tol,
plane_atol=1e-5,
csv_filename=None,
invert_yaxis=False,
cut_type='edge', plot=IS_MATPLOTLIB, show=False)
out = cut_edge_model_by_coord(
model, coord, tol, nodal_result,
plane_atol=1e-5, csv_filename='cut_edge_2.csv')
unused_local_points_array, unused_global_points_array, result_array = out
assert len(result_array) == 20, len(result_array)
unused_geometry_arrays, result_arrays, unused_rods = cut_face_model_by_coord(
model, coord, tol, nodal_result,
plane_atol=1e-5, csv_filename='cut_face_2.csv')
assert len(result_arrays[0]) == 8, len(result_arrays)
os.remove('tris.bdf')
os.remove('cut_edge_2.csv')
os.remove('cut_face_2.csv')
os.remove('plane_edge.bdf')
os.remove('plane_face.bdf')
def test_cut_shell_model_2(self):
"""tests pierce_shell_model"""
tol = 2.
coord = CORD2R(1,
rid=0,
origin=[0.5, 0., 0.],
zaxis=[0.5, 0., 1],
xzplane=[1.5, 0., 0.],
comment='')
model, nodal_result = _cut_shell_model_quads()
#-------------------------------------------------------------------------
# triangles
elements2 = {}
neids = len(model.elements)
for eid, elem in iteritems(model.elements):
elem_a, elem_b = elem.split_to_ctria3(eid, eid + neids)
elements2[elem_a.eid] = elem_a
elements2[elem_b.eid] = elem_b
model.elements = elements2
print(elements2)
model.coords[1] = coord
model.write_bdf('tris.bdf')
print('----------------------------')
local_points_array, global_points_array, result_array = cut_edge_model_by_coord(
model,
coord,
tol,
nodal_result,
plane_atol=1e-5,
csv_filename='cut_edge_2.csv')
assert len(result_array) == 20, len(result_array)
geometry_arrays, result_arrays = cut_face_model_by_coord(
model,
coord,
tol,
nodal_result,
plane_atol=1e-5,
csv_filename='cut_face_2.csv')
assert len(result_arrays[0]) == 8, len(result_arrays)
def plot_shear_moment_torque(model: OP2Geom,
gpforce: RealGridPointForcesArray,
coord: CORD2R,
itime: int=0,
nplanes: int=11, show: bool=True):
nids, nid_cd, xyz_cid0, icd_transform, eids, element_centroids_cid0 = smt_setup(model)
element_centroids_coord = coord.transform_node_to_local_array(element_centroids_cid0)
idir = 0
x = element_centroids_coord[idir]
xmin = x.min()
xmax = x.max()
dx = xmax - xmin
assert abs(dx) > 0., f'dx={dx} xmin={xmin} xmax={xmax}'
stations = np.linspace(0., dx, num=nplanes, endpoint=True)
force_sum, moment_sum, new_coords, nelems, nnodes = gpforce.shear_moment_diagram(
nids, xyz_cid0, nid_cd, icd_transform,
eids, element_centroids_cid0, stations,
model.coords, coord,
iaxis_march=None,
itime=itime, debug=False, log=model.log)
plot_smt(stations, force_sum, moment_sum, nelems, nnodes, show=show)
def get_coords_box(ncuts): # pragma: no cover
dys = []
coords = []
for i in range(ncuts):
dy = -0.1 * i - 0.1 # box
#coord = CORD2R(1, rid=0, origin=[0., dy, 0.], zaxis=[0., dy, 1], xzplane=[1., dy, 0.])
coord = CORD2R(1, rid=0, origin=[0., dy, 0.], zaxis=[0., dy, 1], xzplane=[1., dy, 0.])
#if dy < -5:
#print('break', dy)
#break
#origin = np.array([0., dy, 0.])
#xzplane = origin + dx
#xzplane = np.array([1., dy, 0.])
#coord = CORD2R.add_axes(cid, rid=0, origin=p1, xaxis=p2-p1, yaxis=None, zaxis=None,
#xyplane=None, yzplane=None, xzplane=None, comment='')
#print(coord)
dys.append(dy)
coords.append(coord)
return dys, coords
def test_cut_shell_model_1(self):
"""tests pierce_shell_model"""
model, nodal_result = _cut_shell_model_quads()
coord = CORD2R(1,
rid=0,
origin=[0.5, 0., 0.],
zaxis=[0.5, 0., 1],
xzplane=[1.5, 0., 0.],
comment='')
model.coords[1] = coord
tol = 2.
#-------------------------------------------------------------------------
local_points_array, global_points_array, result_array = cut_edge_model_by_coord(
model, coord, tol, nodal_result, plane_atol=1e-5)
assert len(result_array) == 16, len(result_array)
geometry_array, result_array = cut_face_model_by_coord(model,
coord,
tol,
nodal_result,
plane_atol=1e-5)
assert result_array is None, len(result_array) # no quad support
def test_cord2c_01(self):
"""simple CORD2R/CORD2C input/output test"""
lines = [
'CORD2C* 3 0 0. 0.',
'* 0. 0. 0. 1.*',
'* 1. 0. 1.'
]
model = BDF(debug=False)
card = model.process_card(lines)
cardi = BDFCard(card)
cord2c = CORD2C.add_card(cardi)
model._add_coord_object(cord2c)
lines = [
'CORD2R 4 3 10. 0. 5. 10. 90. 5.',
' 10. 0. 6.'
]
card = model.process_card(lines)
cardi = BDFCard(card)
cord2r = CORD2R.add_card(cardi)
model._add_coord_object(cord2r)
model.cross_reference()
cord2r_b = model.Coord(3)
self.assertEqual(cord2r_b.Cid(), 3)
self.assertEqual(cord2r_b.Rid(), 0)
cord2r_c = model.Coord(4)
self.assertEqual(cord2r_c.Cid(), 4)
self.assertEqual(cord2r_c.Rid(), 3)
self.assertTrue(allclose(cord2r_c.i, array([0., 0., 1.])))
delta = cord2r_c.j - array([1., 1., 0.]) / 2**0.5
self.assertTrue(allclose(cord2r_c.j,
array([1., 1., 0.]) / 2**0.5), str(delta))
delta = cord2r_c.k - array([-1., 1., 0.]) / 2**0.5
self.assertTrue(allclose(cord2r_c.k,
array([-1., 1., 0.]) / 2**0.5), str(delta))
def test_spline2(self):
"""checks the SPLINE2 card"""
#| SPLINE2 | EID | CAERO | ID1 | ID2 | SETG | DZ | DTOR | CID |
#| | DTHX | DTHY | None | USAGE | | | | |
#+---------+------+-------+-------+-------+------+----+------+-----+
#| SPLINE2 | 5 | 8 | 12 | 24 | 60 | 0. | 1.0 | 3 |
#| | 1. | | | | | | | |
cid = 3
origin = [0., 0., 0.]
xaxis = [1., 0., 0.]
xyplane = [0., 1., 0.]
coord = CORD2R.add_axes(cid, rid=0, origin=origin,
xaxis=xaxis, yaxis=None, zaxis=None,
xyplane=xyplane, yzplane=None, xzplane=None,
comment='comment')
eid = 8
pid = 10
cp = 0
nsb = 4
nint = 2
lsb = None
lint = None
p1 = [0., 0., 0.]
x12 = 42.
igid = None
caero2 = CAERO2(eid, pid, igid, p1, x12,
cp=cp, nsb=nsb, nint=nint, lsb=lsb, lint=lint,
comment='this is a caero')
#caero = CAERO2(eid, pid, cp, nsb, nint, lsb, lint, igid, p1, x12)
sid = 60
ids = [7, 13]
set_obj = SET1(sid, ids, is_skin=False, comment='set card')
grid7 = GRID(nid=7, cp=0, xyz=[7., 0., 0.], cd=0, ps='', seid=0, comment='')
grid13 = GRID(nid=13, cp=0, xyz=[13., 0., 0.], cd=0, ps='', seid=0, comment='')
model = BDF(log=None)
model._add_coord_object(coord)
model._add_caero_object(caero2)
model._add_set_object(set_obj)
model._add_node_object(grid7)
model._add_node_object(grid13)
eid = 5
caero = 8
id1 = 12
id2 = 24
setg = 60
dz = 0.
dtor = 1.0
cid = 3
dthx = 1.
dthy = None
usage = None
card = ['SPLINE2', eid, caero, id1, id2, setg, dz, dtor, cid,
dthx, dthy, None, usage]
bdf_card = BDFCard(card, has_none=True)
spline_a = SPLINE2.add_card(bdf_card, comment='spline2_a')
spline_a.write_card()
spline_b = SPLINE2(eid, caero, id1, id2, setg, dz, dtor, cid, dthx,
dthy, usage, comment='spline2_b')
spline_b.validate()
spline_b.write_card()
spline_b.cross_reference(model)
spline_b.write_card()
def test_spline2(self):
"""checks the SPLINE2 card"""
#| SPLINE2 | EID | CAERO | ID1 | ID2 | SETG | DZ | DTOR | CID |
#| | DTHX | DTHY | None | USAGE | | | | |
#+---------+------+-------+-------+-------+------+----+------+-----+
#| SPLINE2 | 5 | 8 | 12 | 24 | 60 | 0. | 1.0 | 3 |
#| | 1. | | | | | | | |
cid = 3
origin = [0., 0., 0.]
xaxis = [1., 0., 0.]
xyplane = [0., 1., 0.]
coord = CORD2R.add_axes(cid, rid=0, origin=origin,
xaxis=xaxis, yaxis=None, zaxis=None,
xyplane=xyplane, yzplane=None, xzplane=None,
comment='comment')
eid = 8
pid = 10
cp = 0
nsb = 4
nint = 2
lsb = None
lint = None
p1 = [0., 0., 0.]
x12 = 42.
igid = None
caero2 = CAERO2(eid, pid, igid, p1, x12,
cp=cp, nsb=nsb, nint=nint, lsb=lsb, lint=lint,
comment='this is a caero')
#caero = CAERO2(eid, pid, cp, nsb, nint, lsb, lint, igid, p1, x12)
sid = 60
ids = [7, 13]
set_obj = SET1(sid, ids, is_skin=False, comment='set card')
grid7 = GRID(nid=7, cp=0, xyz=[7., 0., 0.], cd=0, ps='', seid=0, comment='')
grid13 = GRID(nid=13, cp=0, xyz=[13., 0., 0.], cd=0, ps='', seid=0, comment='')
model = BDF(log=None)
model.add_coord(coord)
model.add_caero(caero2)
model.add_set(set_obj)
model.add_node(grid7)
model.add_node(grid13)
eid = 5
caero = 8
id1 = 12
id2 = 24
setg = 60
dz = 0.
dtor = 1.0
cid = 3
dthx = 1.
dthy = None
usage = None
card = ['SPLINE2', eid, caero, id1, id2, setg, dz, dtor, cid,
dthx, dthy, None, usage]
bdf_card = BDFCard(card, has_none=True)
spline_a = SPLINE2.add_card(bdf_card, comment='spline2_a')
spline_a.write_card()
spline_b = SPLINE2(eid, caero, id1, id2, setg, dz, dtor, cid, dthx,
dthy, usage, comment='spline2_b')
spline_b.validate()
spline_b.write_card()
spline_b.cross_reference(model)
spline_b.write_card()
def test_cut_bwb(self):
"""recover element ids"""
log = SimpleLogger(level='warning', encoding='utf-8', log_func=None)
is_bwb = True
if is_bwb:
bdf_filename = os.path.join(MODEL_PATH, 'bwb',
'bwb_saero.bdf') # ymax~=1262.0
else: # pragma: no cover
bdf_filename = r'C:\NASA\asm\all_modes_mach_0.85\flutter.bdf' # ymax=1160.601
normal_plane = np.array([0., 1., 0.])
model = read_bdf(bdf_filename, log=log)
model2 = read_bdf(bdf_filename, log=log)
# initialize theta
thetas = {}
for eid in model.elements:
# theta, Ex, Ey, Gxy
thetas[eid] = (0., 0., 0., 0.)
#p1 = np.array([466.78845, 735.9053, 0.0])
#p2 = np.array([624.91345, 639.68896, -0.99763656])
#dx = p2 - p1
ytol = 2.
nodal_result = None
plane_bdf_filenames = []
y = []
A = []
I = []
EI = []
avg_centroid = []
for i in range(2000):
if is_bwb:
dy = 100. * i + 1. # bwb
coord = CORD2R(1,
rid=0,
origin=[0., dy, 0.],
zaxis=[0., dy, 1],
xzplane=[1., dy, 0.])
else: # pragma: no cover
dy = 4. * i + 1. # CRM
coord = CORD2R(1,
rid=0,
origin=[0., dy, 0.],
zaxis=[0., dy, 1],
xzplane=[1., dy, 0.])
#origin = np.array([0., dy, 0.])
#xzplane = origin + dx
#xzplane = np.array([1., dy, 0.])
#coord = CORD2R.add_axes(cid, rid=0, origin=p1, xaxis=p2-p1, yaxis=None, zaxis=None,
#xyplane=None, yzplane=None, xzplane=None, comment='')
print(coord)
model.coords[1] = coord
plane_bdf_filename = 'plane_face_%i.bdf' % i
cut_face_filename = 'cut_face_%i.csv' % i
if os.path.exists(cut_face_filename):
os.remove(cut_face_filename)
try:
out = cut_face_model_by_coord(
model2,
coord,
ytol,
nodal_result,
plane_atol=1e-5,
skip_cleanup=True,
#csv_filename=cut_face_filename,
csv_filename=None,
#plane_bdf_filename=None)
plane_bdf_filename=plane_bdf_filename,
plane_bdf_offset=dy)
except RuntimeError:
# incorrect ivalues=[0, 1, 2]; dy=771. for CRM
continue
unused_unique_geometry_array, unused_unique_results_array, rods = out
if not os.path.exists(plane_bdf_filename):
break
plane_bdf_filenames.append(plane_bdf_filename)
# eid, nid, inid1, inid2
#print(unique_geometry_array)
#moi_filename = 'amoi_%i.bdf' % i
moi_filename = None
out = calculate_area_moi(model,
rods,
normal_plane,
thetas,
moi_filename=moi_filename)
#print(out)
Ai, Ii, EIi, avg_centroidi = out
y.append(dy)
A.append(Ai)
I.append(Ii)
EI.append(EIi)
avg_centroid.append(avg_centroidi)
#break
with open('thetas.csv', 'w') as csv_filename:
csv_filename.write('# eid(%i),theta,Ex,Ey,Gxy\n')
for eid, (theta, Ex, Ey, Gxy) in sorted(thetas.items()):
csv_filename.write('%i,%f,%f,%f,%f\n' %
(eid, theta, Ex, Ey, Gxy))
y = np.array(y, dtype='float64')
A = np.array(A, dtype='float64')
I = np.array(I, dtype='float64')
EI = np.array(EI, dtype='float64')
avg_centroid = np.array(avg_centroid, dtype='float64')
inid = 1
beam_model = BDF(debug=False)
avg_centroid[:, 1] = y
# wrong
mid = 1
E = 3.0e7
G = None
nu = 0.3
model.add_mat1(mid, E, G, nu, rho=0.1)
Ix = I[:, 0]
Iy = I[:, 1]
Ixy = I[:, 2]
J = Ix + Iy
#i1, i2, i12 = Ix, Iy, Ixy
for inid, xyz in enumerate(avg_centroid):
beam_model.add_grid(inid + 1, xyz)
for eid in range(1, len(A)):
pid = eid
nids = [eid, eid + 1]
x = [1., 0., 0.]
g0 = None
beam_model.add_cbeam(eid,
pid,
nids,
x,
g0,
offt='GGG',
bit=None,
pa=0,
pb=0,
wa=None,
wb=None,
sa=0,
sb=0,
comment='')
# j = i1 + i2
so = ['YES', 'YES']
xxb = [0., 1.]
area = [A[eid - 1], A[eid]]
i1 = [Ix[eid - 1], Ix[eid]]
i2 = [Iy[eid - 1], Iy[eid]]
i12 = [Ixy[eid - 1], Ixy[eid]]
j = [J[eid - 1], J[eid]]
beam_model.add_pbeam(pid,
mid,
xxb,
so,
area,
i1,
i2,
i12,
j,
nsm=None,
c1=None,
c2=None,
d1=None,
d2=None,
e1=None,
e2=None,
f1=None,
f2=None,
k1=1.,
k2=1.,
s1=0.,
s2=0.,
nsia=0.,
nsib=None,
cwa=0.,
cwb=None,
m1a=0.,
m2a=None,
m1b=0.,
m2b=None,
n1a=0.,
n2a=None,
n1b=0.,
n2b=None,
comment='')
beam_model.write_bdf('equivalent_beam_model.bdf')
X = np.vstack([y, A]).T
Y = np.hstack([X, I, EI, avg_centroid])
header = 'y, A, Ix, Iz, Ixz, Ex*Ix, Ex*Iz, Ex*Ixz, xcentroid, ycentroid, zcentroid'
np.savetxt('cut_data_vs_span.csv', Y, header=header, delimiter=',')
show = True
#show = False
if IS_MATPLOTLIB:
plot_inertia(y, A, I, EI, avg_centroid, show=show)
def test_caero2_1(self):
"""checks the CAERO2/PAERO2/AERO/AEFACT card"""
log = SimpleLogger(level='warning')
model = BDF(log=log)
eid = 1
pid = 10
cp = 4
nsb = 0
nint = 0
lsb = 3
lint = 6
igid = 0
p1 = [0., 1., 2.]
x12 = 10.
caero = CAERO2.add_card(BDFCard(['CAERO2', eid, pid, cp, nsb, nint,
lsb, lint, igid, ] + p1 + [x12]))
#---------------
caero = CAERO2(eid, pid, igid, p1, x12,
cp=cp, nsb=0, nint=nint, lsb=0, lint=lint,
comment='this is a caero')
with self.assertRaises(ValueError):
caero.validate()
caero = CAERO2(eid, pid, igid, p1, x12,
cp=cp, nsb=lsb, nint=0, lsb=lsb, lint=0,
comment='this is a caero')
with self.assertRaises(ValueError):
caero.validate()
#---------------
caero = CAERO2(eid, pid, igid, p1, x12,
cp=cp, nsb=nsb, nint=nint, lsb=lsb, lint=lint,
comment='this is a caero')
caero.validate()
caero.write_card()
aefact = AEFACT.add_card(BDFCard(['AEFACT', lint, 0., 1., 2., 3., 4., 5.]))
aefact = AEFACT(lint, [0., 1., 2., 3., 4., 5.])
aefact.validate()
aefact.write_card()
model.aefacts[lint] = aefact
orient = 'Z'
width = 10.
AR = 2.
lrsb = 0
lrib = 3
lth1 = 0
lth2 = 0
thi = [0]
thn = [0]
paero = PAERO2.add_card(BDFCard(['PAERO2', pid, orient, width, AR,
lrsb, lrib, lth1, lth2] + thi + thn),
comment='paero')
paero = PAERO2(pid, orient, width, AR, lrsb, lrib, lth1, lth2, thi, thn)
paero.validate()
paero.write_card()
model.paeros[pid] = paero
coord = CORD2R.add_card(BDFCard(['CORD2R', cp, 0,
0., 0., 0.,
0., 0., 1.,
1., 0., 0.]))
coord = CORD2R(cp, rid=0, origin=None, zaxis=None, xzplane=None,
comment='')
coord.validate()
model.coords[cp] = coord
aefact = AEFACT(lrib, [0., 1., 2., 3., 4., 5.])
aefact.validate()
model.aefacts[lrib] = aefact
acsid = 0
velocity = None
cref = 1.0
rho_ref = 1.0
aero = AERO.add_card(BDFCard(['AERO', acsid, velocity, cref, rho_ref]))
aero = AERO(velocity, cref, rho_ref, acsid=acsid,
comment='')
aero.validate()
aero.write_card()
model.aero = aero
paero.cross_reference(model)
caero.cross_reference(model)
paero.raw_fields()
caero.raw_fields()
caero.uncross_reference()
caero.raw_fields()
caero.cross_reference(model)
caero.get_points_elements_3d()
caero.get_points()
#caero.get_points_elements_3d()
xyz, elems = caero.get_points_elements_3d()
model.uncross_reference()
model.safe_cross_reference()
model.uncross_reference()
model.write_bdf('aero.temp')
os.remove('aero.temp')
model.cross_reference()
model.write_bdf('aero.temp')
os.remove('aero.temp')
nsb = 4
nint = 2
lsb = None
lint = None
caero2 = CAERO2(eid, pid, igid, p1, x12,
cp=cp, nsb=nsb, nint=nint, lsb=lsb, lint=lint,
comment='this is a caero')
caero2.validate()
caero2.cross_reference(model)
caero2.write_card()
def test_cut_shell_model_2(self):
"""
tests:
- cut_edge_model_by_coord
- cut_face_model_by_coord
"""
tol = 2.
coord = CORD2R(1,
rid=0,
origin=[0.5, 0., 0.],
zaxis=[0.5, 0., 1],
xzplane=[1.5, 0., 0.],
comment='')
model, nodal_result = _cut_shell_model_quads()
#-------------------------------------------------------------------------
# triangles
elements2 = {}
neids = len(model.elements)
for eid, elem in model.elements.items():
elem_a, elem_b = elem.split_to_ctria3(eid, eid + neids)
elements2[elem_a.eid] = elem_a
elements2[elem_b.eid] = elem_b
model.elements = elements2
model.coords[1] = coord
model.write_bdf('tris.bdf')
#print('----------------------------')
title = 'result'
p1 = None
p2 = None
zaxis = None
cut_and_plot_model(title,
p1,
p2,
zaxis,
model,
coord,
nodal_result,
model.log,
tol,
plane_atol=1e-5,
csv_filename=None,
invert_yaxis=False,
cut_type='edge',
show=False)
local_points_array, global_points_array, result_array = cut_edge_model_by_coord(
model,
coord,
tol,
nodal_result,
plane_atol=1e-5,
csv_filename='cut_edge_2.csv')
assert len(result_array) == 20, len(result_array)
geometry_arrays, result_arrays = cut_face_model_by_coord(
model,
coord,
tol,
nodal_result,
plane_atol=1e-5,
csv_filename='cut_face_2.csv')
assert len(result_arrays[0]) == 8, len(result_arrays)
os.remove('tris.bdf')
os.remove('cut_edge_2.csv')
os.remove('cut_face_2.csv')
os.remove('plane_edge.bdf')
os.remove('plane_face.bdf')
def test_cut_shell_model(self):
"""tests pierce_shell_model"""
pid = 10
mid1 = 100
model = BDF(log=log)
# intersects (min)
model.add_grid(1, [0., 0., 0.])
model.add_grid(2, [1., 0., 0.])
model.add_grid(3, [1., 1., 0.])
model.add_grid(4, [0., 1., 0.])
model.add_cquad4(1, pid, [1, 2, 3, 4])
# intersects (max)
model.add_grid(5, [0., 0., 1.])
model.add_grid(6, [1., 0., 1.])
model.add_grid(7, [1., 1., 1.])
model.add_grid(8, [0., 1., 1.])
model.add_cquad4(2, pid, [5, 6, 7, 8])
# intersects (mid)
model.add_grid(9, [0., 0., 0.5])
model.add_grid(10, [1., 0., 0.5])
model.add_grid(11, [1., 1., 0.5])
model.add_grid(12, [0., 1., 0.5])
model.add_cquad4(3, pid, [9, 10, 11, 12])
# doesn't intersect
model.add_grid(13, [10., 0., 0.])
model.add_grid(14, [11., 0., 0.])
model.add_grid(15, [11., 1., 0.])
model.add_grid(16, [10., 1., 0.])
model.add_cquad4(4, pid, [13, 14, 15, 16])
model.add_pshell(pid, mid1=mid1, t=2.)
E = 1.0
G = None
nu = 0.3
model.add_mat1(mid1, E, G, nu, rho=1.0)
model.validate()
model.cross_reference()
xyz_points = [
[0.4, 0.6, 0.],
[-1., -1, 0.],
]
tol = 2.
coord = CORD2R(1,
rid=0,
origin=[0.5, 0., 0.],
zaxis=[0.5, 0., 1],
xzplane=[1.5, 0., 0.],
comment='')
nodal_result = np.linspace(0., 1., num=16)
local_points_array, global_points_array, result_array = cut_edge_model_by_coord(
model, coord, tol, nodal_result, plane_atol=1e-5)
assert len(result_array) == 16, len(result_array)
local_points_array, global_points_array, result_array = cut_face_model_by_coord(
model, coord, tol, nodal_result, plane_atol=1e-5)
assert len(result_array) == 0, len(result_array) # no quad support
def test_caero1_1(self):
"""checks the CAERO1/PAERO1/AEROS/AEFACT card"""
eid = 1
pid = 10
cp = 4
nspan = None
lspan = 3
nchord = None
lchord = 4
igid = 0
p1 = [0., 0., 0.]
x12 = 5.
p4 = [2., 3., 4.]
x43 = 1.
log = SimpleLogger(level='warning')
model = BDF(log=log)
caero = CAERO1.add_card(BDFCard(['CAERO1', eid, pid, cp, nspan, nchord, lspan, lchord,
igid, ] + p1 + [x12] + p4 + [x43]))
caero.validate()
caero = CAERO1.add_card(BDFCard(['CAERO1', eid, pid, None, nspan, nchord, lspan, lchord,
igid, ] + p1 + [x12] + p4 + [x43]))
caero.validate()
caero = CAERO1(eid, pid, cp, nspan, lspan, nchord, lchord, igid, p1,
x12, p4, x43, comment='caero1')
caero.raw_fields()
caero.validate()
caero.write_card()
model.caeros[eid] = caero
p1 = [0., 0., 0.]
p2 = [1., 0., 0.]
p3 = [0.2, 1., 0.]
p4 = [0.1, 1., 0.]
nspan = 5
nchord = 10
igid = -1
caeroq = CAERO1.add_quad(eid, pid, cp, nspan, nchord, igid, p1, p2, p3, p4,
spanwise='y', comment='')
caeroq.validate()
span = 0.1
chord = 0.05
igid = -1
caeroq = CAERO1.add_quad(eid, pid, cp, span, chord, igid, p1, p2, p3, p4,
spanwise='y', comment='')
caeroq.validate()
p1 = [0., 0., 0.]
p2 = [1., 0., 0.]
p3 = [0.2, 0., 1.]
p4 = [0.1, 0., 1.]
span = 0.1
chord = 0.05
igid = -1
caeroq = CAERO1.add_quad(eid, pid, cp, span, chord, igid, p1, p2, p3, p4,
spanwise='z', comment='')
caeroq.validate()
paero = PAERO1(pid, Bi=None, comment='')
paero.validate()
paero.write_card()
model.paeros[pid] = paero
coord = CORD2R(cp, rid=0, origin=None, zaxis=None, xzplane=None,
comment='')
coord.validate()
model.coords[cp] = coord
#acsid = 0.
#velocity = None
cref = 1.0
bref = 2.0
sref = 100.
acsid = 0
rcsid = 0
aeros = AEROS(cref, bref, sref, acsid, rcsid, sym_xz=0, sym_xy=0,
comment='')
aeros.validate()
aeros.write_card()
model.aeros = aeros
aefact = AEFACT(lspan, [0., 1., 2., 3., 4., 5.])
aefact.validate()
model.aefacts[lspan] = aefact
aefact = AEFACT(lchord, [2., 3., 4., 5., 6., 7.])
aefact.validate()
model.aefacts[lchord] = aefact
paero.cross_reference(model)
caero.cross_reference(model)
caero.get_npanel_points_elements()
caero.get_points()
caero.panel_points_elements()
caero.write_card()
model.uncross_reference()
model.cross_reference()
model.uncross_reference()
#model.safe_cross_reference()
caero.safe_cross_reference(model)
caero.panel_points_elements()
caero.raw_fields()
min_max_eid = caero.min_max_eid
self.assertEqual(min_max_eid, [1, 26])
#print('min_eid, max_eid', min_eid, max_eid)
points = [
[0., 0., 0.], # p1
[10., 0., 0.],
[10., 20., 0.],
[5., 20., 0.],
]
caero.set_points(points)
caero.get_points()
str(caero.write_card())
nspan = None
lspan = None
caero = CAERO1(eid, pid, cp, nspan, lspan, nchord, lchord, igid, p1,
x12, p4, x43, comment='caero1')
with self.assertRaises(ValueError):
caero.validate()
nspan = 5
lspan = 5
caero = CAERO1(eid, pid, cp, nspan, lspan, nchord, lchord, igid, p1,
x12, p4, x43, comment='caero1')
with self.assertRaises(ValueError):
caero.validate()
nspan = 5
nchord = None
lchord = None
caero = CAERO1(eid, pid, cp, nspan, lspan, nchord, lchord, igid, p1,
x12, p4, x43, comment='caero1')
with self.assertRaises(ValueError):
caero.validate()
nchord = 10
lchord = 10
caero = CAERO1(eid, pid, cp, nspan, lspan, nchord, lchord, igid, p1,
x12, p4, x43, comment='caero1')
with self.assertRaises(ValueError):
caero.validate()
lspan = None
lchord = None
nspan = 10
nchord = 10
p1 = [0., 0., 0., 0.]
caero = CAERO1(eid, pid, cp, nspan, lspan, nchord, lchord, igid, p1,
x12, p4, x43, comment='caero1')
with self.assertRaises(AssertionError):
caero.validate()
p1 = [0., 0., 0.]
p4 = [1., 2., 3., 4.]
caero = CAERO1(eid, pid, cp, nspan, lspan, nchord, lchord, igid, p1,
x12, p4, x43, comment='caero1')
with self.assertRaises(AssertionError):
caero.validate()
def test_aesurf_1(self):
"""checks the AESURF/AELIST cards"""
aesid = 10
label = 'FLAP'
cid1 = 0
aelist_id1 = 10
cid2 = None
alid2 = None
aesurf1 = AESURF(aesid, label, cid1, aelist_id1, cid2, alid2,
#eff, ldw,
#crefc, crefs, pllim, pulim,
#hmllim, hmulim, tqllim, tqulim,
comment='aesurf comment')
aesurf2 = AESURF.add_card(BDFCard(
[
'AESURF', aesid, label, cid1, aelist_id1, cid2, alid2,
#eff, ldw,
#crefc, crefs, pllim, pulim,
#hmllim, hmulim, tqllim, tqulim,
]), comment='aesurf comment')
#assert aesurf1 == aesurf2
cid2 = 1
coord = CORD2R(cid2, rid=0, origin=[0., 0., 0.],
zaxis=[1., 0., 0.], xzplane=[0., 1., 1.], comment='')
aelist_id1 = 10
aelist_id2 = 20
aesurf2 = AESURF.add_card(BDFCard(
[
'AESURF', aesid, label, cid1, aelist_id1, cid2, aelist_id2,
#eff, ldw,
#crefc, crefs, pllim, pulim,
#hmllim, hmulim, tqllim, tqulim,
]), comment='aesurf comment')
aesurf1.validate()
aesurf2.validate()
log = SimpleLogger(level='warning')
model = BDF()
model._add_coord_object(coord)
model._add_aesurf_object(aesurf1)
elements = [10, 20, 30, 40, 50, 60, 70, 80, 90, 100]
aelist = AELIST(aelist_id1, elements)
model._add_aelist_object(aelist)
elements = [11, 22, 33, 44, 55, 66, 77, 88, 99]
aelist = AELIST(aelist_id2, elements)
model._add_aelist_object(aelist)
aesurf1.cross_reference(model)
aesurf1.write_card()
aesurf1.raw_fields()
aesurf1.uncross_reference()
aesurf1.write_card()
aesurf1.cross_reference(model)
aesurf1.raw_fields()
aesurf2.cross_reference(model)
aesurf2.write_card()
aesurf2.raw_fields()
aesurf2.uncross_reference()
aesurf2.write_card()
aesurf2.cross_reference(model)
aesurf2.raw_fields()
def test_gpforce_01(self):
nids = np.array([1, 2, 3])
xyz_cid0 = np.array([
[1., 1., 1.],
[4., 2., 5.],
[3., 3., 3.],
])
data_code = {
'nonlinear_factor': None,
'sort_bits': [0, 0, 0],
'analysis_code': 1,
'is_msc': True,
'format_code': 1,
'table_code': 1,
'data_names': 'cat',
'device_code': 1,
#'tcode' : 1,
}
is_sort1 = True
isubcase = 1
dt = 0.0
gpforce = RealGridPointForcesArray(data_code, is_sort1, isubcase, dt)
gpforce.ntimes = 1
gpforce.ntotal = 3
gpforce._ntotals = [3]
gpforce.build()
gpforce.data[0, :, :] = np.array([
[
3.,
7.,
11.,
0.,
0.,
0.,
], # fx, fy, fz, mx, my, mz
[
3.,
7.,
11.,
0.,
0.,
0.,
],
[
3.,
7.,
11.,
0.,
0.,
0.,
],
])
gpforce.node_element[0, :, :] = np.array([
[1, 1],
[2, 1],
[3, 1],
])
op2 = OP2()
summation_point = [0., 0., 0.]
i_transform = None
nid_cd = np.array([
[1, 0],
[2, 0],
[3, 0],
])
coord_out = CORD2R(cid=0)
coords = {0: coord_out}
#eids = [1]
#nids = [1]
#gpforce.extract_interface_loads(
#nids, eids, coord_out, coords, nid_cd,
#i_transform,
#xyz_cid0,
#summation_point,
#itime=0,
#debug=True,
#logger=op2.log)
#print('------------')
#eids = [1]
#nids = [2]
#gpforce.extract_interface_loads(
#nids, eids, coord_out, coords, nid_cd,
#i_transform,
#xyz_cid0,
#summation_point,
#itime=0,
#debug=True,
#logger=op2.log)
#print('------------')
eids = [1]
nids = [1, 2]
gpforce.extract_interface_loads(nids,
eids,
coord_out,
coords,
nid_cd,
i_transform,
xyz_cid0,
summation_point,
itime=0,
debug=True,
logger=op2.log)
def test_caero2_1(self):
"""checks the CAERO2/PAERO2/AERO/AEFACT card"""
log = SimpleLogger(level='warning')
model = BDF(log=log)
eid = 1
pid = 10
cp = 4
nsb = 0
nint = 0
lsb = 3
lint = 6
igid = 0
p1 = [0., 1., 2.]
x12 = 10.
caero = CAERO2.add_card(BDFCard(['CAERO2', eid, pid, cp, nsb, nint,
lsb, lint, igid, ] + p1 + [x12]))
#---------------
caero = CAERO2(eid, pid, igid, p1, x12,
cp=cp, nsb=0, nint=nint, lsb=0, lint=lint,
comment='this is a caero')
with self.assertRaises(ValueError):
caero.validate()
caero = CAERO2(eid, pid, igid, p1, x12,
cp=cp, nsb=lsb, nint=0, lsb=lsb, lint=0,
comment='this is a caero')
with self.assertRaises(ValueError):
caero.validate()
#---------------
caero = CAERO2(eid, pid, igid, p1, x12,
cp=cp, nsb=nsb, nint=nint, lsb=lsb, lint=lint,
comment='this is a caero')
caero.validate()
caero.write_card()
aefact = AEFACT.add_card(BDFCard(['AEFACT', lint, 0., 1., 2., 3., 4., 5.]))
aefact = AEFACT(lint, [0., 1., 2., 3., 4., 5.])
aefact.validate()
aefact.write_card()
model.aefacts[lint] = aefact
orient = 'Z'
width = 10.
AR = 2.
lrsb = 0
lrib = 3
lth1 = 0
lth2 = 0
thi = [0]
thn = [0]
paero = PAERO2.add_card(BDFCard(['PAERO2', pid, orient, width, AR,
lrsb, lrib, lth1, lth2] + thi + thn),
comment='paero')
paero = PAERO2(pid, orient, width, AR, lrsb, lrib, lth1, lth2, thi, thn)
paero.validate()
paero.write_card()
model.paeros[pid] = paero
coord = CORD2R.add_card(BDFCard(['CORD2R', cp, 0,
0., 0., 0.,
0., 0., 1.,
1., 0., 0.]))
coord = CORD2R(cp, rid=0, origin=None, zaxis=None, xzplane=None,
comment='')
coord.validate()
model.coords[cp] = coord
aefact = AEFACT(lrib, [0., 1., 2., 3., 4., 5.])
aefact.validate()
model.aefacts[lrib] = aefact
acsid = 0
velocity = None
cref = 1.0
rho_ref = 1.0
aero = AERO.add_card(BDFCard(['AERO', acsid, velocity, cref, rho_ref]))
aero = AERO(velocity, cref, rho_ref, acsid=acsid,
comment='')
aero.validate()
aero.write_card()
model.aero = aero
paero.cross_reference(model)
caero.cross_reference(model)
paero.raw_fields()
caero.raw_fields()
caero.uncross_reference()
caero.raw_fields()
caero.cross_reference(model)
caero.get_points_elements_3d()
caero.get_points()
#caero.get_points_elements_3d()
xyz, elems = caero.get_points_elements_3d()
model.uncross_reference()
model.safe_cross_reference()
model.uncross_reference()
model.write_bdf('aero.temp')
os.remove('aero.temp')
model.cross_reference()
model.write_bdf('aero.temp')
os.remove('aero.temp')
nsb = 4
nint = 2
lsb = None
lint = None
caero2 = CAERO2(eid, pid, igid, p1, x12,
cp=cp, nsb=nsb, nint=nint, lsb=lsb, lint=lint,
comment='this is a caero')
caero2.validate()
caero2.cross_reference(model)
caero2.write_card()