def main():
import numpy
from math import pi, cos, sin
from meshpy.tet import MeshInfo, build
from meshpy.geometry import GeometryBuilder, Marker, \
generate_extrusion, make_box
from meshpy.naca import generate_naca
geob = GeometryBuilder()
box_marker = Marker.FIRST_USER_MARKER
wing_length = 2
wing_subdiv = 5
rz_points = [
(0, -wing_length * 1.05),
(0.7, -wing_length * 1.05),
] + [(r, x) for x, r in zip(
numpy.linspace(-wing_length, 0, wing_subdiv, endpoint=False),
numpy.linspace(0.8, 1, wing_subdiv, endpoint=False))] + [(1, 0)] + [
(r, x) for x, r in zip(
numpy.linspace(wing_length, 0, wing_subdiv, endpoint=False),
numpy.linspace(0.8, 1, wing_subdiv, endpoint=False))
][::-1] + [(0.7, wing_length * 1.05), (0, wing_length * 1.05)]
geob.add_geometry(*generate_extrusion(
rz_points=rz_points,
base_shape=generate_naca("0012", verbose=False, number_of_points=20),
ring_markers=(wing_subdiv * 2 + 4) * [box_marker]))
from meshpy.tools import make_swizzle_matrix
swizzle_matrix = make_swizzle_matrix("z:x,y:y,x:z")
geob.apply_transform(lambda p: numpy.dot(swizzle_matrix, p))
def deform_wing(p):
x, y, z = p
return numpy.array([
x, y + 0.1 * abs(x / wing_length)**2,
z + 0.8 * abs(x / wing_length)**1.2
])
geob.apply_transform(deform_wing)
points, facets, _, facet_markers = make_box(
numpy.array([-wing_length - 1, -1, -1.5]),
numpy.array([wing_length + 1, 1, 3]))
geob.add_geometry(points, facets, facet_markers=facet_markers)
mesh_info = MeshInfo()
geob.set(mesh_info)
mesh_info.set_holes([(0, 0, 0.5)])
mesh = build(mesh_info)
print "%d elements" % len(mesh.elements)
mesh.write_vtk("airfoil3d.vtk")
from matplotlib import pylab as plt
from mpl_toolkits.mplot3d import Axes3D
from meshpy.tet import MeshInfo, build
rz = [(0, 0), (1, 0), (1.5, 0.5), (2, 1), (0, 1)]
base = []
for theta in np.linspace(0, 2 * np.pi, 40):
x = np.sin(theta)
y = np.cos(theta)
base.extend([(x, y)])
(points, facets, facet_holestarts,
markers) = generate_extrusion(rz_points=rz, base_shape=base)
p_array = np.array(points)
xs = p_array[:, 0]
ys = p_array[:, 1]
zs = p_array[:, 2]
fig = plt.figure()
ax = fig.add_subplot(111, projection='3d')
ax.scatter(xs, ys, zs)
for f in facets:
plt.plot(xs[list(f[0])], ys[list(f[0])], zs[list(f[0])])
plt.show()
for i_facet, poly_list in enumerate(facets):
print(poly_list)
def make_wingmesh():
import numpy
from math import pi, cos, sin
from meshpy.tet import MeshInfo, build
from meshpy.geometry import GeometryBuilder, Marker, \
generate_extrusion, make_box
geob = GeometryBuilder()
profile_marker = Marker.FIRST_USER_MARKER
wing_length = 2
wing_subdiv = 5
rz_points = [
(0, -wing_length * 1.05),
(0.7, -wing_length * 1.05),
] + [(r, x) for x, r in zip(
numpy.linspace(-wing_length, 0, wing_subdiv, endpoint=False),
numpy.linspace(0.8, 1, wing_subdiv, endpoint=False))] + [(1, 0)] + [
(r, x) for x, r in zip(
numpy.linspace(wing_length, 0, wing_subdiv, endpoint=False),
numpy.linspace(0.8, 1, wing_subdiv, endpoint=False))
][::-1] + [(0.7, wing_length * 1.05), (0, wing_length * 1.05)]
from meshpy.naca import get_naca_points
geob.add_geometry(*generate_extrusion(
rz_points=rz_points,
base_shape=get_naca_points("0012", number_of_points=20),
ring_markers=(wing_subdiv * 2 + 4) * [profile_marker]))
def deform_wing(p):
x, y, z = p
return numpy.array([
x + 0.8 * abs(z / wing_length)**1.2,
y + 0.1 * abs(z / wing_length)**2, z
])
geob.apply_transform(deform_wing)
points, facets, facet_markers = make_box(
numpy.array([-1.5, -1, -wing_length - 1], dtype=numpy.float64),
numpy.array([3, 1, wing_length + 1], dtype=numpy.float64))
geob.add_geometry(points, facets, facet_markers=facet_markers)
mesh_info = MeshInfo()
geob.set(mesh_info)
mesh_info.set_holes([(0.5, 0, 0)])
mesh = build(mesh_info)
print("%d elements" % len(mesh.elements))
fvi2fm = mesh.face_vertex_indices_to_face_marker
face_marker_to_tag = {
profile_marker: "noslip",
Marker.MINUS_X: "inflow",
Marker.PLUS_X: "outflow",
Marker.MINUS_Y: "inflow",
Marker.PLUS_Y: "inflow",
Marker.PLUS_Z: "inflow",
Marker.MINUS_Z: "inflow"
}
def bdry_tagger(fvi, el, fn, all_v):
face_marker = fvi2fm[fvi]
return [face_marker_to_tag[face_marker]]
from grudge.mesh import make_conformal_mesh
return make_conformal_mesh(mesh.points, mesh.elements, bdry_tagger)
def make_wingmesh():
import numpy
from math import pi, cos, sin
from meshpy.tet import MeshInfo, build
from meshpy.geometry import GeometryBuilder, Marker, \
generate_extrusion, make_box
geob = GeometryBuilder()
profile_marker = Marker.FIRST_USER_MARKER
wing_length = 2
wing_subdiv = 5
rz_points = [
(0, -wing_length*1.05),
(0.7, -wing_length*1.05),
] + [
(r, x) for x, r in zip(
numpy.linspace(-wing_length, 0, wing_subdiv, endpoint=False),
numpy.linspace(0.8, 1, wing_subdiv, endpoint=False))
] + [(1,0)] + [
(r, x) for x, r in zip(
numpy.linspace(wing_length, 0, wing_subdiv, endpoint=False),
numpy.linspace(0.8, 1, wing_subdiv, endpoint=False))
][::-1] + [
(0.7, wing_length*1.05),
(0, wing_length*1.05)
]
from meshpy.naca import get_naca_points
geob.add_geometry(*generate_extrusion(
rz_points=rz_points,
base_shape=get_naca_points("0012", number_of_points=20),
ring_markers=(wing_subdiv*2+4)*[profile_marker]))
def deform_wing(p):
x, y, z = p
return numpy.array([
x + 0.8*abs(z/wing_length)** 1.2,
y + 0.1*abs(z/wing_length)**2,
z])
geob.apply_transform(deform_wing)
points, facets, facet_markers = make_box(
numpy.array([-1.5,-1,-wing_length-1], dtype=numpy.float64),
numpy.array([3,1,wing_length+1], dtype=numpy.float64))
geob.add_geometry(points, facets, facet_markers=facet_markers)
mesh_info = MeshInfo()
geob.set(mesh_info)
mesh_info.set_holes([(0.5,0,0)])
mesh = build(mesh_info)
print "%d elements" % len(mesh.elements)
fvi2fm = mesh.face_vertex_indices_to_face_marker
face_marker_to_tag = {
profile_marker: "noslip",
Marker.MINUS_X: "inflow",
Marker.PLUS_X: "outflow",
Marker.MINUS_Y: "inflow",
Marker.PLUS_Y: "inflow",
Marker.PLUS_Z: "inflow",
Marker.MINUS_Z: "inflow"
}
def bdry_tagger(fvi, el, fn, all_v):
face_marker = fvi2fm[fvi]
return [face_marker_to_tag[face_marker]]
from hedge.mesh import make_conformal_mesh
return make_conformal_mesh(mesh.points, mesh.elements, bdry_tagger)
def generateConeMesh(plot=True):
x0 = 0
y0 = 0
z0 = 1
h = 1
r_bottom = 1.3
r_top = 1.5
r_scale = r_top / r_bottom
rz = [(0, z0),
(1, z0),
(r_scale, z0 + h),
(0, z0 + h)]
base = []
# Create circle
for theta in np.linspace(0, 2 * np.pi, 40):
x = r_bottom * np.sin(theta)
y = r_bottom * np.cos(theta)
base.extend([(x, y)])
(points, facets,
facet_holestarts, markers) = generate_extrusion(rz_points=rz,
base_shape=base)
if plot:
p_array = np.array(points)
xs = p_array[:, 0] + x0
ys = p_array[:, 1] + y0
zs = p_array[:, 2]
fig = plt.figure()
ax = fig.add_subplot(111, projection='3d')
ax.scatter(xs, ys, zs)
for f in facets:
plt.plot(xs[list(f[0])], ys[list(f[0])], zs[list(f[0])])
if True:
axLim = ax.get_w_lims()
MAX = np.max(axLim)
for direction in (-1, 1):
for point in np.diag(direction * MAX * np.array([1, 1, 1])):
ax.plot(
[point[0]], [point[1]], [np.abs(point[2])], 'w')
x = [0, 0]
y = [0, 0]
z = [1, 1 + 0.2]
plt.plot(x, y, z)
plt.show()
mesh_info = MeshInfo()
mesh_info.set_points(points)
mesh_info.set_facets_ex(facets)
mesh = build(mesh_info)
# print(mesh.elements)
cellList = []
vertexList = []
mupifMesh = Mesh.UnstructuredMesh()
for i, p in enumerate(mesh.points):
p = (p[0] + x0, p[1] + y0, p[2])
vertexList.extend([Vertex.Vertex(i, i, p)])
for i, t in enumerate(mesh.elements):
cellList.extend([Cell.Tetrahedron_3d_lin(mupifMesh, i, i, t)])
mupifMesh.setup(vertexList, cellList)
return(mupifMesh)
def main():
import numpy
#from math import pi, cos, sin
from meshpy.tet import MeshInfo, build
from meshpy.geometry import GeometryBuilder, Marker, \
generate_extrusion, make_box
from meshpy.naca import get_naca_points
geob = GeometryBuilder()
box_marker = Marker.FIRST_USER_MARKER
wing_length = 2
wing_subdiv = 5
rz_points = [
(0, -wing_length*1.05),
(0.7, -wing_length*1.05),
] + [
(r, x) for x, r in zip(
numpy.linspace(-wing_length, 0, wing_subdiv, endpoint=False),
numpy.linspace(0.8, 1, wing_subdiv, endpoint=False))
] + [(1, 0)] + [
(r, x) for x, r in zip(
numpy.linspace(wing_length, 0, wing_subdiv, endpoint=False),
numpy.linspace(0.8, 1, wing_subdiv, endpoint=False))
][::-1] + [
(0.7, wing_length*1.05),
(0, wing_length*1.05)
]
geob.add_geometry(*generate_extrusion(
rz_points=rz_points,
base_shape=get_naca_points("0012", verbose=False, number_of_points=20),
ring_markers=(wing_subdiv*2+4)*[box_marker]))
from meshpy.tools import make_swizzle_matrix
swizzle_matrix = make_swizzle_matrix("z:x,y:y,x:z")
geob.apply_transform(lambda p: numpy.dot(swizzle_matrix, p))
def deform_wing(p):
x, y, z = p
return numpy.array([
x,
y + 0.1*abs(x/wing_length)**2,
z + 0.8*abs(x/wing_length) ** 1.2])
geob.apply_transform(deform_wing)
points, facets, _, facet_markers = make_box(
numpy.array([-wing_length-1, -1, -1.5]),
numpy.array([wing_length+1, 1, 3]))
geob.add_geometry(points, facets, facet_markers=facet_markers)
mesh_info = MeshInfo()
geob.set(mesh_info)
mesh_info.set_holes([(0, 0, 0.5)])
mesh = build(mesh_info)
print("%d elements" % len(mesh.elements))
mesh.write_vtk("airfoil3d.vtk")
def generateConeMesh(plot=True):
x0 = 0
y0 = 0
z0 = 1
h = 1
r_bottom = 1.3
r_top = 1.5
r_scale = r_top / r_bottom
rz = [(0, z0), (1, z0), (r_scale, z0 + h), (0, z0 + h)]
base = []
# Create circle
for theta in np.linspace(0, 2 * np.pi, 40):
x = r_bottom * np.sin(theta)
y = r_bottom * np.cos(theta)
base.extend([(x, y)])
(points, facets, facet_holestarts,
markers) = generate_extrusion(rz_points=rz, base_shape=base)
if plot:
p_array = np.array(points)
xs = p_array[:, 0] + x0
ys = p_array[:, 1] + y0
zs = p_array[:, 2]
fig = plt.figure()
ax = fig.add_subplot(111, projection='3d')
ax.scatter(xs, ys, zs)
for f in facets:
plt.plot(xs[list(f[0])], ys[list(f[0])], zs[list(f[0])])
if True:
axLim = ax.get_w_lims()
MAX = np.max(axLim)
for direction in (-1, 1):
for point in np.diag(direction * MAX * np.array([1, 1, 1])):
ax.plot([point[0]], [point[1]], [np.abs(point[2])], 'w')
x = [0, 0]
y = [0, 0]
z = [1, 1 + 0.2]
plt.plot(x, y, z)
plt.show()
mesh_info = MeshInfo()
mesh_info.set_points(points)
mesh_info.set_facets_ex(facets)
mesh = build(mesh_info)
# print(mesh.elements)
cellList = []
vertexList = []
mupifMesh = Mesh.UnstructuredMesh()
for i, p in enumerate(mesh.points):
p = (p[0] + x0, p[1] + y0, p[2])
vertexList.extend([Vertex.Vertex(i, i, p)])
for i, t in enumerate(mesh.elements):
cellList.extend([Cell.Tetrahedron_3d_lin(mupifMesh, i, i, t)])
mupifMesh.setup(vertexList, cellList)
return (mupifMesh)
from mpl_toolkits.mplot3d import Axes3D
from meshpy.tet import MeshInfo, build
rz = [(0, 0), (1, 0), (1.5, 0.5), (2, 1), (0, 1)]
base = []
for theta in np.linspace(0, 2 * np.pi, 40):
x = np.sin(theta)
y = np.cos(theta)
base.extend([(x, y)])
(points, facets,
facet_holestarts, markers) = generate_extrusion(rz_points=rz, base_shape=base)
p_array = np.array(points)
xs = p_array[:, 0]
ys = p_array[:, 1]
zs = p_array[:, 2]
fig = plt.figure()
ax = fig.add_subplot(111, projection='3d')
ax.scatter(xs, ys, zs)
for f in facets:
plt.plot(xs[list(f[0])], ys[list(f[0])], zs[list(f[0])])
plt.show()