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Study of the NASA/LANGLEY LS(1)-0417 (GA(W)-1) Airfoil - Copy
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1 Geometry
4 Meshes
4 Simulation setups
9 Results
1 Geometry 4 Meshes 4 Simulation setups 9 ResultsAbout this project
Measurement of the lift coefficient and drag coefficient at a certain angle of attack. - Copy
