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Study of the NASA/LANGLEY LS(1)-0417 (GA(W)-1) Airfoil
1105
5
Statistics
1 Geometry
3 Meshes
3 Simulation setups
7 Results
1 Geometry 3 Meshes 3 Simulation setups 7 ResultsAbout this project
Measurement of the lift coefficient and drag coefficient at a certain angle of attack.
