diff --git a/dart/api/core.py b/dart/api/core.py
index af1922a94c01469f6d82753f1d9a2526028339d3..8359e35b75e2f6d53ff24ec03bb9c6cd26a4cee2 100644
--- a/dart/api/core.py
+++ b/dart/api/core.py
@@ -122,17 +122,21 @@ def initDart(cfg, scenario='aerodynamic', task='analysis'):
if _dim == 2:
mshCrck = tbox.MshCrack(_msh, _dim)
mshCrck.setCrack(cfg['Wake'])
- mshCrck.addBoundaries([cfg['Fluid'], cfg['Farfield'][-1], cfg['Wing']])
+ mshCrck.addBoundary(cfg['Fluid'])
+ mshCrck.addBoundary(cfg['Farfield'][-1])
+ mshCrck.addBoundary(cfg['Wing'])
mshCrck.run()
else:
for i in range(len(cfg['Wakes'])):
mshCrck = tbox.MshCrack(_msh, _dim)
mshCrck.setCrack(cfg['Wakes'][i])
- mshCrck.addBoundaries([cfg['Fluid'], cfg['Farfield'][-1], cfg['Wings'][i]])
+ mshCrck.addBoundary(cfg['Fluid'])
+ mshCrck.addBoundary(cfg['Farfield'][-1])
+ mshCrck.addBoundary(cfg['Wings'][i])
if 'Fuselage' in cfg:
- mshCrck.addBoundaries([cfg['Fuselage']])
+ mshCrck.addBoundary(cfg['Fuselage'])
if 'Symmetry' in cfg:
- mshCrck.addBoundaries([cfg['Symmetry']])
+ mshCrck.addBoundary(cfg['Symmetry'])
if 'WakeTips' in cfg:
mshCrck.setExcluded(cfg['WakeTips'][i]) # 3D computations (not excluded for 2.5D)
mshCrck.run()
@@ -146,20 +150,22 @@ def initDart(cfg, scenario='aerodynamic', task='analysis'):
if scenario == 'aerostructural' or task == 'optimization':
_mrf = tbox.MshDeform(_msh, tbox.Gmres(1, 1e-6, 30, 1e-8), _dim, nthrds=nthrd, vrb=verb)
_mrf.setField(cfg['Fluid'])
- _mrf.addFixed(cfg['Farfield'])
+ for tag in cfg['Farfield']:
+ _mrf.addFixed(tag)
if _dim == 2:
- _mrf.addMoving([cfg['Wing']])
- _mrf.addInternal([cfg['Wake'], cfg['Wake']+'_'])
+ _mrf.addMoving(cfg['Wing'])
+ _mrf.addInternal(cfg['Wake'], cfg['Wake']+'_')
else:
if 'Fuselage' in cfg:
_mrf.addFixed(cfg['Fuselage'])
- _mrf.setSymmetry(cfg['Symmetry'], 1)
+ if 'Symmetry' in cfg:
+ _mrf.setSymmetry(cfg['Symmetry'], 1)
for i in range(len(cfg['Wings'])):
if i == 0:
- _mrf.addMoving([cfg['Wings'][i]]) # TODO body of interest (FSI/OPT) is always first given body
+ _mrf.addMoving(cfg['Wings'][i]) # TODO body of interest (FSI/OPT) is always first given body
else:
- _mrf.addFixed([cfg['Wings'][i]])
- _mrf.addInternal([cfg['Wakes'][i], cfg['Wakes'][i]+'_'])
+ _mrf.addFixed(cfg['Wings'][i])
+ _mrf.addInternal(cfg['Wakes'][i], cfg['Wakes'][i]+'_')
_mrf.initialize()
else:
_mrf = None
diff --git a/dart/default.py b/dart/default.py
index ba0be480c2a35461791e2546099731738a849d2a..2a05db4c7d7df4fea350cfbbccf08e48559e4686 100644
--- a/dart/default.py
+++ b/dart/default.py
@@ -23,7 +23,7 @@ from fwk.wutils import parseargs
import dart
import tbox
-def mesh(dim, file, pars, bnd, wk = 'wake', wktp = None):
+def mesh(dim, file, pars, bnds, wk = 'wake', wktp = None):
"""Initialize mesh and mesh writer
Parameters
@@ -34,7 +34,7 @@ def mesh(dim, file, pars, bnd, wk = 'wake', wktp = None):
file contaning mesh (w/o extention)
pars : dict
parameters for mesh
- bnd : array of str
+ bnds : array of str
names of crack (wake) boundaries physical tag
wk : str (optional)
name of crack (wake) physical tag
@@ -47,7 +47,8 @@ def mesh(dim, file, pars, bnd, wk = 'wake', wktp = None):
# crack the mesh
mshCrck = tbox.MshCrack(msh, dim)
mshCrck.setCrack(wk)
- mshCrck.addBoundaries(bnd)
+ for bnd in bnds:
+ mshCrck.addBoundary(bnd)
if dim == 3 and wktp is not None:
mshCrck.setExcluded(wktp)
mshCrck.run()
@@ -189,11 +190,12 @@ def morpher(msh, dim, mov, fxd = ['upstream', 'farfield', 'downstream'], fld = '
args = parseargs()
mshDef = tbox.MshDeform(msh, tbox.Gmres(1, 1e-6, 30, 1e-8), dim, nthrds=args.k)
mshDef.setField(fld)
- mshDef.addFixed(fxd)
+ for tag in fxd:
+ mshDef.addFixed(tag)
mshDef.addMoving(mov)
if dim == 3:
mshDef.setSymmetry(sym, 1)
- mshDef.addInternal([wk, wk+'_'])
+ mshDef.addInternal(wk, wk+'_')
mshDef.initialize()
return mshDef
diff --git a/dart/tests/adjoint.py b/dart/tests/adjoint.py
index f2ed009ed4f7fd00b350dbd6ac2f5c01a09c63b3..df03af2e7fec29ae787f34edacad6ee37b71cc28 100644
--- a/dart/tests/adjoint.py
+++ b/dart/tests/adjoint.py
@@ -50,7 +50,7 @@ def main():
pars = {'xLgt' : 5, 'yLgt' : 5, 'msF' : 1., 'msTe' : 0.0075, 'msLe' : 0.0075}
msh, gmshWriter = floD.mesh(dim, 'models/n0012.geo', pars, ['field', 'airfoil', 'downstream'])
# create mesh deformation handler
- morpher = floD.morpher(msh, dim, ['airfoil'])
+ morpher = floD.morpher(msh, dim, 'airfoil')
tms['msh'].stop()
# set the problem and add fluid, initial/boundary conditions
diff --git a/dart/tests/morpher.py b/dart/tests/morpher.py
index 63c9b47408f4652c440fc871545f7d5e24c685a9..5bca5c11e4ebff7b62457edeb725c770d69267ba 100644
--- a/dart/tests/morpher.py
+++ b/dart/tests/morpher.py
@@ -55,7 +55,7 @@ def main():
pars = {'xLgt' : 5, 'yLgt' : 5, 'msF' : 1., 'msTe' : 0.01, 'msLe' : 0.01}
msh, gmshWriter = floD.mesh(dim, 'models/n0012.geo', pars, ['field', 'airfoil', 'downstream'])
# create mesh deformation handler
- morpher = floD.morpher(msh, dim, ['airfoil'])
+ morpher = floD.morpher(msh, dim, 'airfoil')
# mesh the reference geometry
pars = {'xLgt' : 5, 'yLgt' : 5, 'msF' : 1., 'msTe' : 0.01, 'msLe' : 0.01, 'angle' : alfa, 'xRot' : xc}
msh_ref, gmshWriter_ref = floD.mesh(dim, 'models/n0012.geo', pars, ['field', 'airfoil', 'downstream'])
diff --git a/dart/tests/rae_25.py b/dart/tests/rae_25.py
index 33a83b483196a1f19ac55efe1b89b6ed49a73eb1..95ab324502dc9d1614f0822c89e69e3e4e92001a 100644
--- a/dart/tests/rae_25.py
+++ b/dart/tests/rae_25.py
@@ -56,7 +56,7 @@ def main():
tms["msh"].start()
pars = {'spn' : spn, 'lgt' : lgt, 'wdt' : wdt, 'hgt' : hgt, 'msN' : nms, 'msF' : fms}
msh, gmshWriter = floD.mesh(dim, 'models/rae_25.geo', pars, ['field', 'wing', 'symmetry', 'downstream'])
- morpher = floD.morpher(msh, dim, ['wing'])
+ morpher = floD.morpher(msh, dim, 'wing')
tms["msh"].stop()
# set the problem and add fluid, initial/boundary conditions
diff --git a/dart/tests/rae_3.py b/dart/tests/rae_3.py
index 7bb85ba18422030359f68f4a983fb93046752545..72097ac0e1d1cd7fae6b3d8b3020db89edbaa5fa 100644
--- a/dart/tests/rae_3.py
+++ b/dart/tests/rae_3.py
@@ -61,7 +61,7 @@ def main():
tms["msh"].start()
pars = {'spn' : spn, 'lgt' : lgt, 'wdt' : wdt, 'hgt' : hgt, 'msN' : nms, 'msF' : fms}
msh, gmshWriter = floD.mesh(dim, 'models/rae_3.geo', pars, ['field', 'wing', 'symmetry', 'downstream'], wktp = 'wakeTip')
- morpher = floD.morpher(msh, dim, ['wing'])
+ morpher = floD.morpher(msh, dim, 'wing')
tms["msh"].stop()
# set the problem and add fluid, initial/boundary conditions
diff --git a/dart/validation/agard.py b/dart/validation/agard.py
index fb1fb03e48dbaf7e1dd78c8e89b0b3021f136581..dc18dcb7da37bdbb618c3cf05c12763a1338a6f5 100644
--- a/dart/validation/agard.py
+++ b/dart/validation/agard.py
@@ -84,7 +84,7 @@ def main():
tms['post'].start()
if canPost:
floU.writeSlices(msh.name,[0.01, 0.37, 0.75],5)
- data = tbxU.read('slice_1.dat')
+ data = tbxU.read('agard445_slice_1.dat')
tbxU.plot(data[:,3], data[:,4], 'x', 'Cp', 'Pressure distribution at MAC', True)
tms['post'].stop()
diff --git a/dart/validation/onera.py b/dart/validation/onera.py
index 8bb1fadc0f30c4603fe088c1f5345aec76212979..85f4e671a9b9e8164e463fdefa2fe6e7a69f5d5a 100644
--- a/dart/validation/onera.py
+++ b/dart/validation/onera.py
@@ -82,7 +82,7 @@ def main():
tms['post'].start()
if canPost:
floU.writeSlices(msh.name,[0.01, 0.239, 0.526, 0.777, 0.957, 1.076, 1.136, 1.184],5)
- data = tbxU.read('slice_2.dat')
+ data = tbxU.read('oneraM6_slice_2.dat')
tbxU.plot(data[:,3], data[:,4], 'x', 'Cp', 'Pressure distribution at MAC', True)
tms['post'].stop()
diff --git a/ext/amfe b/ext/amfe
index 7dbafd30acd41e369b54962af8a0994af1aa55e8..7a60afc9668ac6793c98f76ef79835158769c662 160000
--- a/ext/amfe
+++ b/ext/amfe
@@ -1 +1 @@
-Subproject commit 7dbafd30acd41e369b54962af8a0994af1aa55e8
+Subproject commit 7a60afc9668ac6793c98f76ef79835158769c662