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High Aspect Ratio Wing - Copy
1
0
Statistics
2 Geometries
4 Meshes
1 Simulation setup
3 Results
2 Geometries 4 Meshes 1 Simulation setup 3 ResultsAbout this project
Evaluation of high aspect ratio wing with incompressible CFD results and comparison to 2D airfoil results. AR of 67.26457, cord of 0.44600, airfoil is NLF(1)-0215F - Copy
