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Study of the NASA/LANGLEY LS(1)-0417 (GA(W)-1) Airfoil - Copy
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1Â Geometry
4Â Meshes
4Â Simulation setups
7Â Results
1Â Geometry 4Â Meshes 4Â Simulation setups 7Â ResultsAbout this project
Measurement of the lift coefficient and drag coefficient at a certain angle of attack. - Copy
