From 90b9c6064653d49a854cdb9e58b9d49c37e37d90 Mon Sep 17 00:00:00 2001
From: Paul Dechamps <paul.dechamps@uliege.be>
Date: Thu, 27 Feb 2025 18:43:06 +0100
Subject: [PATCH] (feat) Modify test case for data structures modifications
---
blast/tests/dart/t_rae2822_3D.py | 3 ++-
blast/tests/t_sections_3D.py | 2 +-
blast/validation/v_rae2822_2D.py | 4 ++--
3 files changed, 5 insertions(+), 4 deletions(-)
diff --git a/blast/tests/dart/t_rae2822_3D.py b/blast/tests/dart/t_rae2822_3D.py
index f58d79b..b4018f5 100644
--- a/blast/tests/dart/t_rae2822_3D.py
+++ b/blast/tests/dart/t_rae2822_3D.py
@@ -175,6 +175,7 @@ def main():
from matplotlib import pyplot as plt
for icp in range(len(cpi)):
+ blaster_nodes = isol.vBnd[0][icp][0].getNodes('all')
plt.figure()
plt.plot(cpi[icp][:, 0], cpi[icp][:, 2], label='Inviscid')
plt.plot(cpv[icp][:, 0], cpv[icp][:, 2], label='Viscous')
@@ -184,7 +185,7 @@ def main():
plt.legend()
plt.draw()
plt.figure()
- plt.plot(isol.vBnd[0][icp][0].nodesCoord[:,0], isol.vBnd[0][icp][0].nodesCoord[:,2], '-', label='Paulzer')
+ plt.plot(blaster_nodes[:,0], blaster_nodes[:,2], '-', label='BLASTER')
plt.plot(cpi[icp][:, 0], cpi[icp][:, 1], '--', label='VTK')
plt.legend()
plt.axis('equal')
diff --git a/blast/tests/t_sections_3D.py b/blast/tests/t_sections_3D.py
index 75d015e..e2e8070 100644
--- a/blast/tests/t_sections_3D.py
+++ b/blast/tests/t_sections_3D.py
@@ -133,7 +133,7 @@ def main():
tms[gen_section].stop()
for isec in range(len(vcfg['sections']['wing'])):
- wing_sections[imethod].append(copy.deepcopy(isol.vBnd[0][isec][0].nodesCoord))
+ wing_sections[imethod].append(copy.deepcopy(isol.vBnd[0][isec][0].getNodes('all')))
del isol
tms['total'].stop()
diff --git a/blast/validation/v_rae2822_2D.py b/blast/validation/v_rae2822_2D.py
index e812ca6..7a6f15b 100644
--- a/blast/validation/v_rae2822_2D.py
+++ b/blast/validation/v_rae2822_2D.py
@@ -87,7 +87,7 @@ def cfgBlast(verb):
'couplTol' : 1e-4, # Tolerance of the VII methodology
'iterPrint': 1, # int, number of iterations between outputs
'resetInv' : True, # bool, flag to reset the inviscid calculation at every iteration.
- 'sections' : [0],
+ 'sections' : {'airfoil': [0]},
'xtrF' : [0.03, 0.03],# Forced transition location
'interpolator' : 'Matching',
'nDim' : 2
@@ -124,7 +124,7 @@ def main():
print('{0:6.1f}e6 {1:8.2f} {2:8.1f} {3:8.4f} {4:8.4f} {5:8.4f} {6:8.4f} {7:8.4f}'.format(vcfg['Re']/1e6, isol.getMinf(), isol.getAoA()*180/math.pi, isol.getCl(), vsol.Cdt, vsol.Cdp, vsol.Cdf, isol.getCm()))
# Write results to file.
- vSolution = vutils.getSolution(isol.sec)
+ vSolution = vutils.getSolution(vsol.bodies[0].sections)[0]
tms['total'].stop()
print(ccolors.ANSI_BLUE + 'PyTiming...' + ccolors.ANSI_RESET)
--
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