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Hello,
I want to use an airfoil that is not a NACA section.
As far as I understand, I need to pass the call() function with airfoil='name of the file'.
However, when I do so I get the following…
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Hi!
I am trying to simulate a wind turbine with dirty blades, so I would like to modify the polar curve of airfoils. When I use AirfoilPrep to expand the drag coefficient, I need to estimate CDmax th…
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Hey.
I don't know anything about 3D-printing and OpenSCAD, but I do know stuff about airfoils and aerodynamics. I am wondering how it would be possible to implement the usage of NACA-profiles / air…
MaNyh updated
4 months ago
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In the given example of NREL5MW, have the data cl and cd of airfoil DU21 been tested and verified when Re=7000000 or Re=6000000? Is there any experimental data to support it?
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I want to use this solver for airfoil simulation but get an error, when I use this solver for rhoPimpleFoam's airfoil case. What further changes to the boundary conditions must be made.
Thank You
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While debugging some differences in a new method of calculating default unsteady airfoil coefficients, I noticed some unusual characteristics in the lift coefficients in several of the aerodyn/BAR_Bas…
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In the current prototype of the `naca` app, the airfoil is described [using sampled edges](https://github.com/solvcon/modmesh/blob/bc9e26f07585d74b2fb4d96c194ff209e7c78996/modmesh/app/naca.py#L104). …
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Stefanino, I'm back to this after a long hiatus. My apologies, but I'm having trouble again.
I had previously processed leparagliding7_36AR7.txt (https://drive.google.com/file/d/1PD7ccab-fCqPNpCIy_b…
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```
What steps will reproduce the problem?
1. play thru an airport express using Airfoil
2. using the IR remote to play/pause, skip the tracks and change the volume
What is the expected output?
pla…
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the metroliners center of gravity is to far forward