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cruise missile test 11
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Statistics
1 Geometry
3 Meshes
1 Simulation setup
2 Results
1 Geometry 3 Meshes 1 Simulation setup 2 ResultsAbout this project
root airfoil unscaled (1:1 with original) bottom max thickness point 35mm from leading edge sweep back offset changed to 60mm or 13.5 degrees (trailing edge no sweep) wing length increased to 250mm
