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Study of the NASA/LANGLEY LS(1)-0417 (GA(W)-1) Airfoil - Copy
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1 Geometry 3 Meshes 1 Simulation setup 1 Result
About this project
Measurement of the lift coefficient and drag coefficient at a certain angle of attack. - Copy
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by Ali_ArafatAli_Arafat
Project History
Bernie created this project
dald copied this project