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Dear libAcoustics developers,
Using your library, I can only simulate less than one second due to an error that I present in what follows:
`[0] #0 Foam::error::printStack(Foam::Ostream&) at ??:…
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I am currently using tigl wrapper for python/matlab, the tigl.wingGetWettedArea(wingUID) gives problem while tigl.wingGetSpan(wingUID) is fine. Does anyone have any idea why? Version tigl 2.2.3, tixi …
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I'm interested in creating a 3D airfoil from a set of points. My plan is to make multiple planes with different NACA equations on each plane and then loft them together. For example, the first plane w…
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As an operator of Patadmin I want to mark a critical patient. The flag if a patient is critical can be changed while editing a patient. A critical patient is shown differently in the usage overview of…
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When I open the included naca msh file in latest gmsh, no mesh is displayed. I also dont get any error in gmsh. Do you know what could be wrong ?
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I am getting following error while installing meshpy
My python version is
conda version : 4.5.11
conda-build version : 3.10.5
python version : 3.6.5.final.0
++++++++++++++++++++++…
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Hi,
I'm trying to convert some p3d meshes generated by the Construct2D code ([https://sourceforge.net/projects/construct2d/](https://sourceforge.net/projects/construct2d/)) up with a GMSH file of …
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Dear all,
In the CalculateDistanceToSkinProcess2D, which was recently added to the master branch, the distance is computed in the elements that are intersecting the skin model part. The rest of the…
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@dany93
I found that the airfoil which the Cessna 172P uses is the NACA2412.
See
http://www.airfoildb.com/airfoils/356
for a lift polar / drag polar.
I have four or five documents here …
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A number of tests fail or give deprecation warning when running in FullDebug (from the full suite)
also the test_KratosCore is now taking far too long. A naca0012 distance calculation test has been…