Set up your own cloud-native simulation in minutes.Start Simulating Now
Study of the NASA/LANGLEY LS(1)-0417 (GA(W)-1) Airfoil
491
2
Statistics
1 Geometry
3 Meshes
1 Simulation setup
1 Result
1 Geometry 3 Meshes 1 Simulation setup 1 ResultAbout this project
Measurement of the lift coefficient and drag coefficient at a certain angle of attack.
Related Projects
Project History
Bernie created this project
about 5 years ago
