def meshStructure(self, res, filename):
afm = Airframe(self, res)
idims = numpy.linspace(0.45, 0.9, 7)
jdims = numpy.linspace(0, 1, 16)
for i in range(idims.shape[0] - 1):
for j in range(jdims.shape[0]):
afm.addVertFlip('Mlw_1:' + str(i) + ':' + str(j), 'wing',
[idims[i], jdims[j]], [idims[i + 1], jdims[j]])
for i in range(idims.shape[0]):
for j in range(jdims.shape[0] - 1):
if i is 0 or i is idims.shape[0] - 1:
afm.addVertFlip('Mlw_2:' + str(i) + ':' + str(j), 'wing',
[idims[i], jdims[j]],
[idims[i], jdims[j + 1]])
else:
afm.addVertFlip('Mlw_2a:' + str(i) + ':' + str(j),
'wing', [idims[i], jdims[j]],
[idims[i], jdims[j + 1]],
w=[1, 0.85])
afm.addVertFlip('Mlw_2b:' + str(i) + ':' + str(j),
'wing', [idims[i], jdims[j]],
[idims[i], jdims[j + 1]],
w=[0.15, 0])
idims = numpy.linspace(0.18, 0.45, 6)
for j in range(idims.shape[0] - 1):
afm.addVertFlip('Mlw_sec1:' + str(j), 'wing', [idims[j], jdims[j]],
[idims[j + 1], jdims[j + 1]])
afm.addVertFlip('Mlw_sec2:' + str(j), 'wing', [idims[j], jdims[j]],
[0.45, jdims[j]])
afm.preview('wing_pvw.dat')
afm.mesh()
afm.computeMesh(filename + '_str.dat')
def meshStructure(self):
afm = Airframe(self, 4)
idims = numpy.linspace(0.25,0.65,7)
jdims = numpy.linspace(0.02,0.36,16)
for i in range(idims.shape[0]-1):
for j in range(jdims.shape[0]):
afm.addVertFlip('Mlw_1:'+str(i)+':'+str(j),'HWB',[idims[i],jdims[j]],[idims[i+1],jdims[j]])
afm.addVertFlip('Mrw_1:'+str(i)+':'+str(j),'HWB',[idims[i],1-jdims[j]],[idims[i+1],1-jdims[j]])
for i in range(idims.shape[0]):
for j in range(jdims.shape[0]-1):
if i is 0 or i is idims.shape[0]-1:
afm.addVertFlip('Mlw_2:'+str(i)+':'+str(j),'HWB',[idims[i],jdims[j]],[idims[i],jdims[j+1]])
afm.addVertFlip('Mrw_2:'+str(i)+':'+str(j),'HWB',[idims[i],1-jdims[j]],[idims[i],1-jdims[j+1]])
else:
afm.addVertFlip('Mlw_2a:'+str(i)+':'+str(j),'HWB',[idims[i],jdims[j]],[idims[i],jdims[j+1]],w=[1,0.85])
afm.addVertFlip('Mlw_2b:'+str(i)+':'+str(j),'HWB',[idims[i],jdims[j]],[idims[i],jdims[j+1]],w=[0.15,0])
afm.addVertFlip('Mrw_2a:'+str(i)+':'+str(j),'HWB',[idims[i],1-jdims[j]],[idims[i],1-jdims[j+1]],w=[1,0.85])
afm.addVertFlip('Mrw_2b:'+str(i)+':'+str(j),'HWB',[idims[i],1-jdims[j]],[idims[i],1-jdims[j+1]],w=[0.15,0])
ind = self.inds
def run(v1,v2,v3):
a = 0.2
b = 0.75
jdims = numpy.linspace(a,b,7)
for j in range(jdims.shape[0]-1):
afm.addMember(name,[
[[ind['HWB'], 0,0], [1,jdims[j],v1], [1,jdims[j+1],v1], [0.8,jdims[j],v2], [0.8,jdims[j+1],v2]],
[[ind['HWB'], 1,0], [0,1-jdims[j],v1], [0,1-jdims[j+1],v1], [0.2,1-jdims[j],v2], [0.2,1-jdims[j+1],v2]],
])
afm.addMember(name,[
[[ind['HWB'], 0,0], [1,jdims[j],v3+0], [1,jdims[j+1],v3+0], [0.8,jdims[j],v2], [0.8,jdims[j+1],v2]],
[[ind['HWB'], 1,0], [0,1-jdims[j],v3+0], [0,1-jdims[j+1],v3+0], [0.2,1-jdims[j],v2], [0.2,1-jdims[j+1],v2]],
])
afm.addMember(name,[
[[ind['HWB'], 0,0], [0,jdims[j],v1], [0,jdims[j+1],v1], [0.2,jdims[j],v2], [0.2,jdims[j+1],v2]],
[[ind['HWB'], 1,0], [1,1-jdims[j],v1], [1,1-jdims[j+1],v1], [0.8,1-jdims[j],v2], [0.8,1-jdims[j+1],v2]],
])
afm.addMember(name,[
[[ind['HWB'], 0,0], [0,jdims[j],v3+0], [0,jdims[j+1],v3+0], [0.2,jdims[j],v2], [0.2,jdims[j+1],v2]],
[[ind['HWB'], 1,0], [1,1-jdims[j],v3+0], [1,1-jdims[j+1],v3+0], [0.8,1-jdims[j],v2], [0.8,1-jdims[j+1],v2]],
])
afm.addMember(name,[
[[ind['HWB'], 0,0], [0.8,jdims[j],v2], [0.8,jdims[j+1],v2], [0.2,jdims[j],v2], [0.2,jdims[j+1],v2]],
[[ind['HWB'], 1,0], [0.2,1-jdims[j],v2], [0.2,1-jdims[j+1],v2], [0.8,1-jdims[j],v2], [0.8,1-jdims[j+1],v2]],
])
#run(0.36,0.37,0.387)
#run(0.43,0.45,0.477)
#run(0.53,0.55,0.577)
#run(0.62,0.63,0.647)
run(0.36,0.37,0.38)
run(0.43,0.45,0.47)
run(0.53,0.55,0.57)
run(0.62,0.63,0.64)
afm.preview('HWB_pvw.dat')
afm.mesh()
afm.computeMesh('HWB_str.dat')
def meshStructure(self, res, filename):
afm = Airframe(self, res)
idims = numpy.linspace(0.45,0.9,7)
jdims = numpy.linspace(0,1,16)
for i in range(idims.shape[0]-1):
for j in range(jdims.shape[0]):
afm.addVertFlip('Mlw_1:'+str(i)+':'+str(j),'wing',[idims[i],jdims[j]],[idims[i+1],jdims[j]])
for i in range(idims.shape[0]):
for j in range(jdims.shape[0]-1):
if i is 0 or i is idims.shape[0]-1:
afm.addVertFlip('Mlw_2:'+str(i)+':'+str(j),'wing',[idims[i],jdims[j]],[idims[i],jdims[j+1]])
else:
afm.addVertFlip('Mlw_2a:'+str(i)+':'+str(j),'wing',[idims[i],jdims[j]],[idims[i],jdims[j+1]],w=[1,0.85])
afm.addVertFlip('Mlw_2b:'+str(i)+':'+str(j),'wing',[idims[i],jdims[j]],[idims[i],jdims[j+1]],w=[0.15,0])
idims = numpy.linspace(0.18,0.45,6)
for j in range(idims.shape[0]-1):
afm.addVertFlip('Mlw_sec1:'+str(j),'wing',[idims[j],jdims[j]],[idims[j+1],jdims[j+1]])
afm.addVertFlip('Mlw_sec2:'+str(j),'wing',[idims[j],jdims[j]],[0.45,jdims[j]])
afm.preview('wing_pvw.dat')
afm.mesh()
afm.computeMesh(filename + '_str.dat')
def meshStructure(self):
afm = Airframe(self, 0.2)
idims = numpy.linspace(0.45,0.85,7)
jdims = numpy.linspace(0,0.9,16)
for i in range(idims.shape[0]-1):
for j in range(jdims.shape[0]):
afm.addVertFlip('Mlw_1:'+str(i)+':'+str(j),'lw',[idims[i],jdims[j]],[idims[i+1],jdims[j]])
afm.addVertFlip('Mrw_1:'+str(i)+':'+str(j),'rw',[idims[i],1-jdims[j]],[idims[i+1],1-jdims[j]])
for i in range(idims.shape[0]):
for j in range(jdims.shape[0]-1):
if i is 0 or i is idims.shape[0]-1:
afm.addVertFlip('Mlw_2:'+str(i)+':'+str(j),'lw',[idims[i],jdims[j]],[idims[i],jdims[j+1]])
afm.addVertFlip('Mrw_2:'+str(i)+':'+str(j),'rw',[idims[i],1-jdims[j]],[idims[i],1-jdims[j+1]])
else:
afm.addVertFlip('Mlw_2a:'+str(i)+':'+str(j),'lw',[idims[i],jdims[j]],[idims[i],jdims[j+1]],w=[1,0.85])
afm.addVertFlip('Mlw_2b:'+str(i)+':'+str(j),'lw',[idims[i],jdims[j]],[idims[i],jdims[j+1]],w=[0.15,0])
afm.addVertFlip('Mrw_2a:'+str(i)+':'+str(j),'rw',[idims[i],1-jdims[j]],[idims[i],1-jdims[j+1]],w=[1,0.85])
afm.addVertFlip('Mrw_2b:'+str(i)+':'+str(j),'rw',[idims[i],1-jdims[j]],[idims[i],1-jdims[j+1]],w=[0.15,0])
idims = numpy.linspace(0.18,0.45,6)
for j in range(idims.shape[0]-1):
afm.addVertFlip('Mlw_sec1:'+str(j),'lw',[idims[j],jdims[j]],[idims[j+1],jdims[j+1]])
afm.addVertFlip('Mrw_sec1:'+str(j),'rw',[idims[j],1-jdims[j]],[idims[j+1],1-jdims[j+1]])
afm.addVertFlip('Mlw_sec2:'+str(j),'lw',[idims[j],jdims[j]],[0.45,jdims[j]])
afm.addVertFlip('Mrw_sec2:'+str(j),'rw',[idims[j],1-jdims[j]],[0.45,1-jdims[j]])
idims = numpy.linspace(0.45,0.85,7)
jdims = numpy.linspace(0,0.9,16)
for i in range(idims.shape[0]):
if i is 0 or i is idims.shape[0]-1:
afm.addCtrVert('Mcw_2:'+str(i)+':'+str(j),'lw','rw',idims[i])
else:
afm.addCtrVert('Mcw_2a:'+str(i)+':'+str(j),'lw','rw',idims[i],w=[1,0.85])
afm.addCtrVert('Mcw_2b:'+str(i)+':'+str(j),'lw','rw',idims[i],w=[0.15,0])
for i in range(idims.shape[0]-1):
afm.addCtr('Mcw_u:','lw','rw',0,[idims[i],idims[i+1]])
for i in range(idims.shape[0]-1):
afm.addCtr('Mcw_l:','lw','rw',1,[1-idims[i],1-idims[i+1]])
afm.addCtrVert('Mcw_sec:'+str(i)+':'+str(j),'lw','rw',0.18)
idims = numpy.linspace(0.25,0.65,2)
jdims = numpy.linspace(0,0.9,10)
for i in range(idims.shape[0]-1):
for j in range(jdims.shape[0]):
afm.addVertFlip('Mlt_1:'+str(i)+':'+str(j),'lt',[idims[i],jdims[j]],[idims[i+1],jdims[j]])
afm.addVertFlip('Mrt_1:'+str(i)+':'+str(j),'rt',[idims[i],1-jdims[j]],[idims[i+1],1-jdims[j]])
afm.addVertFlip('Mvt_1:'+str(i)+':'+str(j),'vt',[idims[i],jdims[j]],[idims[i+1],jdims[j]])
for i in range(idims.shape[0]):
for j in range(jdims.shape[0]-1):
afm.addVertFlip('Mlt_2:'+str(i)+':'+str(j),'lt',[idims[i],jdims[j]],[idims[i],jdims[j+1]])
afm.addVertFlip('Mrt_2:'+str(i)+':'+str(j),'rt',[idims[i],1-jdims[j]],[idims[i],1-jdims[j+1]])
afm.addVertFlip('Mvt_2:'+str(i)+':'+str(j),'vt',[idims[i],jdims[j]],[idims[i],jdims[j+1]])
for i in range(idims.shape[0]):
afm.addCtrVert('Mct_2:'+str(i)+':'+str(j),'lt','rt',idims[i])
for i in range(idims.shape[0]-1):
afm.addCtr('Mct_u:','lt','rt',0,[idims[i],idims[i+1]])
for i in range(idims.shape[0]-1):
afm.addCtr('Mct_l:','lt','rt',1,[1-idims[i],1-idims[i+1]])
idims = numpy.linspace(0,1,4)
jdims = numpy.linspace(0,1,20)
for i in range(idims.shape[0]-1):
for j in range(jdims.shape[0]):
afm.addVert('Mfu_1:'+str(i)+':'+str(j),'fu',[idims[i],jdims[j]],[idims[i+1],jdims[j]],w=[1.0,0.94],i=[0,2])
afm.addVert('Mfu_2:'+str(i)+':'+str(j),'fu',[idims[i],jdims[j]],[idims[i+1],jdims[j]],w=[1.0,0.94],i=[1,3])
afm.addVert('Mfu_3:'+str(i)+':'+str(j),'fu',[idims[i],jdims[j]],[idims[i+1],jdims[j]],w=[1.0,0.94],i=[2,0])
afm.addVert('Mfu_4:'+str(i)+':'+str(j),'fu',[idims[i],jdims[j]],[idims[i+1],jdims[j]],w=[1.0,0.94],i=[3,1])
for i in range(idims.shape[0]):
for j in range(jdims.shape[0]-1):
afm.addVert('Mfu_5:'+str(i)+':'+str(j),'fu',[idims[i],jdims[j]],[idims[i],jdims[j+1]],w=[1.0,0.97],i=[0,2])
afm.addVert('Mfu_6:'+str(i)+':'+str(j),'fu',[idims[i],jdims[j]],[idims[i],jdims[j+1]],w=[1.0,0.97],i=[1,3])
afm.addVert('Mfu_7:'+str(i)+':'+str(j),'fu',[idims[i],jdims[j]],[idims[i],jdims[j+1]],w=[1.0,0.97],i=[2,0])
afm.addVert('Mfu_8:'+str(i)+':'+str(j),'fu',[idims[i],jdims[j]],[idims[i],jdims[j+1]],w=[1.0,0.97],i=[3,1])
for j in range(jdims.shape[0]-1):
afm.addVertFlip('Mfu_0:'+str(j),'fu',[0.4,jdims[j]],[0.4,jdims[j+1]],w=[1.0,0.0],i=[0,2])
afm.preview('conventional_pvw.dat')
afm.mesh()
afm.computeMesh('conventional_str.dat')
def meshStructure(this, filename):
afm = Airframe(this, 1)
middle_spar = 11
hinge_spar = 5
hinge_location = 0.22 # 0.285
#idims = np.array([ 0.08, 0.15, 0.22, hinge_location, 0.3875, 0.49, 0.5925, 0.695, 0.7975, 0.9])
# idims = np.linspace(0.08,0.9,9) #13
idims = np.append(
np.linspace(0.08, hinge_location, 5)[0:-1],
np.linspace(hinge_location, 0.9, 14))
angle_rib = 3
angle_location = 0.55 #20.0/37.0 #this.wing_width_section_1/this.wing_width_section_2 # + 0.05 #########
jdims = np.array([0.0, 0.18333333, angle_location, 0.7, 0.85, 1.0])
# jdims = np.append(np.linspace(0,angle_location,4)[0:-1],np.linspace(angle_location,1,4)) #13
for i in range(idims.shape[0] - 1):
for j in range(jdims.shape[0]):
if i < hinge_spar and j < 1: continue
afm.addVertFlip('MRIBW:%02d:l:%02d' % (j, i), 'lwing',
[idims[i], jdims[j]], [idims[i + 1], jdims[j]])
afm.addVertFlip('MRIBW:%02d:r:%02d' % (j, i), 'rwing',
[idims[i], 1 - jdims[j]],
[idims[i + 1], 1 - jdims[j]])
for i in range(idims.shape[0]):
for j in range(jdims.shape[0] - 1):
if i < hinge_spar and j < 1: continue
if i in [0, hinge_spar, idims.shape[0] - 1]: # middle_spar,
afm.addVertFlip('MSPARW:%02d:l:%02d' % (i, j), 'lwing',
[idims[i], jdims[j]],
[idims[i], jdims[j + 1]])
afm.addVertFlip('MSPARW:%02d:r:%02d' % (i, j), 'rwing',
[idims[i], 1 - jdims[j]],
[idims[i], 1 - jdims[j + 1]])
else:
if i in [6, 8, 10, 12, 14, 16] and j >= angle_rib - 1:
continue
afm.addVertFlip('MSTRINGW:%02d:a:l:%02d' % (i, j),
'lwing', [idims[i], jdims[j]],
[idims[i], jdims[j + 1]],
w=[1, 0.85])
afm.addVertFlip('MSTRINGW:%02d:b:l:%02d' % (i, j),
'lwing', [idims[i], jdims[j]],
[idims[i], jdims[j + 1]],
w=[0.15, 0])
afm.addVertFlip('MSTRINGW:%02d:a:r:%02d' % (i, j),
'rwing', [idims[i], 1 - jdims[j]],
[idims[i], 1 - jdims[j + 1]],
w=[1, 0.85])
afm.addVertFlip('MSTRINGW:%02d:b:r:%02d' % (i, j),
'rwing', [idims[i], 1 - jdims[j]],
[idims[i], 1 - jdims[j + 1]],
w=[0.15, 0])
for i in range(hinge_spar, idims.shape[0]):
if i in [hinge_spar, idims.shape[0] - 1]:
afm.addCtrVert('MSPARC:%02d' % (i), 'lwing', 'rwing', idims[i])
else:
afm.addCtrVert('MSTRINGC:%02d:a' % (i),
'lwing',
'rwing',
idims[i],
w=[1, 0.85])
afm.addCtrVert('MSTRINGC:%02d:b' % (i),
'lwing',
'rwing',
idims[i],
w=[0.15, 0])
for i in range(hinge_spar, idims.shape[0] - 1):
afm.addCtr('MSKINC:a:%02d' % (i), 'lwing', 'rwing', 0,
[idims[i], idims[i + 1]])
for i in range(hinge_spar, idims.shape[0] - 1):
afm.addCtr('MSKINC:b:%02d' % (i), 'lwing', 'rwing', 1,
[1 - idims[i], 1 - idims[i + 1]])
if this.tail:
idims = np.array([0.2, 0.4, 0.6, 0.8])
jdims = np.linspace(0.0, 0.95, 10)
for i in range(idims.shape[0] - 1):
for j in range(jdims.shape[0]):
afm.addVertFlip('MRIBV:%02d:%02d' % (j, i), 'ctail',
[idims[i], jdims[j]],
[idims[i + 1], jdims[j]])
for i in range(idims.shape[0]):
for j in range(jdims.shape[0] - 1):
afm.addVertFlip('MSPARV:%02d:%02d' % (i, j), 'ctail',
[idims[i], jdims[j]],
[idims[i], jdims[j + 1]])
idims = np.linspace(0.15, 0.85, 4)
jdims = np.linspace(0.0, 1.0, 8)
for i in range(idims.shape[0] - 1):
for j in range(jdims.shape[0]):
afm.addVertFlip('MRIBF:%02d:%02d' % (j, i), 'flap',
[idims[i], jdims[j]], [idims[i + 1], jdims[j]])
for i in range(idims.shape[0]):
for j in range(jdims.shape[0] - 1):
afm.addVertFlip('MSPARF:%02d:%02d' % (i, j), 'flap',
[idims[i], jdims[j]], [idims[i], jdims[j + 1]])
jdims = np.linspace(0, 1, 20) # 13
idims = np.linspace(0, 1, 5)
for i in range(idims.shape[0] - 1):
for j in range(jdims.shape[0]):
afm.addVert('MFRAME:%02d:1:%02d' % (j, i),
'fuse', [idims[i], jdims[j]],
[idims[i + 1], jdims[j]],
w=[1.0, 0.96],
i=[0, 2])
afm.addVert('MFRAME:%02d:3:%02d' % (j, i),
'fuse', [idims[i], jdims[j]],
[idims[i + 1], jdims[j]],
w=[1.0, 0.96],
i=[2, 0])
for i in range(idims.shape[0] - 1):
for j in range(jdims.shape[0] - 1):
afm.addVert('MLONG:%02d:1:%02d' % (i, j),
'fuse', [idims[i], jdims[j]],
[idims[i], jdims[j + 1]],
w=[1.0, 0.96],
i=[0, 2])
afm.addVert('MLONG:%02d:3:%02d' % (i, j),
'fuse', [idims[i], jdims[j]],
[idims[i], jdims[j + 1]],
w=[1.0, 0.96],
i=[2, 0])
idims = np.linspace(0, 1, 6)
for i in range(idims.shape[0] - 1):
for j in range(jdims.shape[0]):
afm.addVert('MFRAME:%02d:2:%02d' % (j, i),
'fuse', [idims[i], jdims[j]],
[idims[i + 1], jdims[j]],
w=[1.0, 0.96],
i=[1, 3])
for i in range(idims.shape[0] - 1):
for j in range(jdims.shape[0] - 1):
afm.addVert('MLONG:%02d:2:%02d' % (i, j),
'fuse', [idims[i], jdims[j]],
[idims[i], jdims[j + 1]],
w=[1.0, 0.96],
i=[1, 3])
idims = np.linspace(0, 1, 10)
for i in range(idims.shape[0] - 1):
for j in range(jdims.shape[0]):
afm.addVert('MFRAME:%02d:4:%02d' % (j, i),
'fuse', [idims[i], jdims[j]],
[idims[i + 1], jdims[j]],
w=[1.0, 0.96],
i=[3, 1])
for i in range(idims.shape[0] - 1):
for j in range(jdims.shape[0] - 1):
afm.addVert('MLONG:%02d:4:%02d' % (i, j),
'fuse', [idims[i], jdims[j]],
[idims[i], jdims[j + 1]],
w=[1.0, 0.96],
i=[3, 1])
afm.preview('preview')
afm.mesh()
afm.computeMesh(filename)
def meshStructure(self):
afm = Airframe(self, 1) #0.2)
idims = numpy.linspace(0.45, 0.9, 7)
jdims = numpy.linspace(0, 1, 16)
for i in range(idims.shape[0] - 1):
for j in range(jdims.shape[0]):
afm.addVertFlip('Mlw_1:' + str(i) + ':' + str(j), 'lwing',
[idims[i], jdims[j]], [idims[i + 1], jdims[j]])
afm.addVertFlip('Mrw_1:' + str(i) + ':' + str(j), 'rwing',
[idims[i], 1 - jdims[j]],
[idims[i + 1], 1 - jdims[j]])
for i in range(idims.shape[0]):
for j in range(jdims.shape[0] - 1):
if i is 0 or i is idims.shape[0] - 1:
afm.addVertFlip('Mlw_2:' + str(i) + ':' + str(j), 'lwing',
[idims[i], jdims[j]],
[idims[i], jdims[j + 1]])
afm.addVertFlip('Mrw_2:' + str(i) + ':' + str(j), 'rwing',
[idims[i], 1 - jdims[j]],
[idims[i], 1 - jdims[j + 1]])
else:
afm.addVertFlip('Mlw_2a:' + str(i) + ':' + str(j),
'lwing', [idims[i], jdims[j]],
[idims[i], jdims[j + 1]],
w=[1, 0.85])
afm.addVertFlip('Mlw_2b:' + str(i) + ':' + str(j),
'lwing', [idims[i], jdims[j]],
[idims[i], jdims[j + 1]],
w=[0.15, 0])
afm.addVertFlip('Mrw_2a:' + str(i) + ':' + str(j),
'rwing', [idims[i], 1 - jdims[j]],
[idims[i], 1 - jdims[j + 1]],
w=[1, 0.85])
afm.addVertFlip('Mrw_2b:' + str(i) + ':' + str(j),
'rwing', [idims[i], 1 - jdims[j]],
[idims[i], 1 - jdims[j + 1]],
w=[0.15, 0])
idims = numpy.linspace(0.18, 0.45, 6)
for j in range(idims.shape[0] - 1):
afm.addVertFlip('Mlw_sec1:' + str(j), 'lwing',
[idims[j], jdims[j]], [idims[j + 1], jdims[j + 1]])
afm.addVertFlip('Mrw_sec1:' + str(j), 'rwing',
[idims[j], 1 - jdims[j]],
[idims[j + 1], 1 - jdims[j + 1]])
afm.addVertFlip('Mlw_sec2:' + str(j), 'lwing',
[idims[j], jdims[j]], [0.45, jdims[j]])
afm.addVertFlip('Mrw_sec2:' + str(j), 'rwing',
[idims[j], 1 - jdims[j]], [0.45, 1 - jdims[j]])
idims = numpy.linspace(0.45, 0.85, 7)
jdims = numpy.linspace(0, 1, 16)
for i in range(idims.shape[0]):
if i is 0 or i is idims.shape[0] - 1:
afm.addCtrVert('Mcw_2:' + str(i) + ':' + str(j), 'lwing',
'rwing', idims[i])
else:
afm.addCtrVert('Mcw_2a:' + str(i) + ':' + str(j),
'lwing',
'rwing',
idims[i],
w=[1, 0.85])
afm.addCtrVert('Mcw_2b:' + str(i) + ':' + str(j),
'lwing',
'rwing',
idims[i],
w=[0.15, 0])
for i in range(idims.shape[0] - 1):
afm.addCtr('Mcw_u:', 'lwing', 'rwing', 0, [idims[i], idims[i + 1]])
for i in range(idims.shape[0] - 1):
afm.addCtr('Mcw_l:', 'lwing', 'rwing', 1,
[1 - idims[i], 1 - idims[i + 1]])
afm.addCtrVert('Mcw_sec:' + str(i) + ':' + str(j), 'lwing', 'rwing',
0.18)
idims = numpy.linspace(0.25, 0.65, 2)
jdims = numpy.linspace(0, 0.9, 10)
for i in range(idims.shape[0] - 1):
for j in range(jdims.shape[0]):
afm.addVertFlip('Mlt_1:' + str(i) + ':' + str(j), 'ltail',
[idims[i], jdims[j]], [idims[i + 1], jdims[j]])
afm.addVertFlip('Mrt_1:' + str(i) + ':' + str(j), 'rtail',
[idims[i], 1 - jdims[j]],
[idims[i + 1], 1 - jdims[j]])
afm.addVertFlip('Mvt_1:' + str(i) + ':' + str(j), 'vtail',
[idims[i], jdims[j]], [idims[i + 1], jdims[j]])
for i in range(idims.shape[0]):
for j in range(jdims.shape[0] - 1):
afm.addVertFlip('Mlt_2:' + str(i) + ':' + str(j), 'ltail',
[idims[i], jdims[j]], [idims[i], jdims[j + 1]])
afm.addVertFlip('Mrt_2:' + str(i) + ':' + str(j), 'rtail',
[idims[i], 1 - jdims[j]],
[idims[i], 1 - jdims[j + 1]])
afm.addVertFlip('Mvt_2:' + str(i) + ':' + str(j), 'vtail',
[idims[i], jdims[j]], [idims[i], jdims[j + 1]])
for i in range(idims.shape[0]):
afm.addCtrVert('Mct_2:' + str(i) + ':' + str(j), 'ltail', 'rtail',
idims[i])
for i in range(idims.shape[0] - 1):
afm.addCtr('Mct_u:', 'ltail', 'rtail', 0, [idims[i], idims[i + 1]])
for i in range(idims.shape[0] - 1):
afm.addCtr('Mct_l:', 'ltail', 'rtail', 1,
[1 - idims[i], 1 - idims[i + 1]])
idims = numpy.linspace(0, 1, 4)
jdims = numpy.linspace(0, 1, 20)
for i in range(idims.shape[0] - 1):
for j in range(jdims.shape[0]):
afm.addVert('Mfu_F1:' + str(i) + ':' + str(j),
'fuse', [idims[i], jdims[j]],
[idims[i + 1], jdims[j]],
w=[1.0, 0.94],
i=[0, 2])
afm.addVert('Mfu_F2:' + str(i) + ':' + str(j),
'fuse', [idims[i], jdims[j]],
[idims[i + 1], jdims[j]],
w=[1.0, 0.94],
i=[1, 3])
afm.addVert('Mfu_F3:' + str(i) + ':' + str(j),
'fuse', [idims[i], jdims[j]],
[idims[i + 1], jdims[j]],
w=[1.0, 0.94],
i=[2, 0])
afm.addVert('Mfu_F4:' + str(i) + ':' + str(j),
'fuse', [idims[i], jdims[j]],
[idims[i + 1], jdims[j]],
w=[1.0, 0.94],
i=[3, 1])
for i in range(idims.shape[0] - 1):
for j in range(jdims.shape[0] - 1):
afm.addVert('Mfu_L1:' + str(i) + ':' + str(j),
'fuse', [idims[i], jdims[j]],
[idims[i], jdims[j + 1]],
w=[1.0, 0.97],
i=[0, 2])
afm.addVert('Mfu_L2:' + str(i) + ':' + str(j),
'fuse', [idims[i], jdims[j]],
[idims[i], jdims[j + 1]],
w=[1.0, 0.97],
i=[1, 3])
afm.addVert('Mfu_L3:' + str(i) + ':' + str(j),
'fuse', [idims[i], jdims[j]],
[idims[i], jdims[j + 1]],
w=[1.0, 0.97],
i=[2, 0])
afm.addVert('Mfu_L4:' + str(i) + ':' + str(j),
'fuse', [idims[i], jdims[j]],
[idims[i], jdims[j + 1]],
w=[1.0, 0.97],
i=[3, 1])
for j in range(jdims.shape[0] - 1):
afm.addVertFlip('Mfu_0a:' + str(j),
'fuse', [0.4, jdims[j]], [0.4, jdims[j + 1]],
w=[1.0, 0.5],
i=[0, 2])
afm.addVertFlip('Mfu_0b:' + str(j),
'fuse', [0.4, jdims[j]], [0.4, jdims[j + 1]],
w=[0.5, 0.0],
i=[0, 2])
afm.preview('conventional_pvw.dat')
afm.mesh()
afm.computeMesh('conventional_str.dat')