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conv 20 aoa 10 - Copy - Copy
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2 Geometries
1 Mesh
1 Simulation setup
2 Results
2 Geometries 1 Mesh 1 Simulation setup 2 ResultsAbout this project
cfd analysis of a conventional airfoil at a 20 degree flap angle - Copy - Copy
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Abeth created this project
bhandari_mohak copied this project