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cruise missile test 10 - Copy
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1 Geometry
1 Mesh
1 Simulation setup
3 Results
1 Geometry 1 Mesh 1 Simulation setup 3 ResultsAbout this project
after realizing the need of agility, and the need to improve lift, airfoil change- bottom max thick is moved to be 28mm from leading edge. span increased to 240mm new sweep back angle is 21.4, offset still 100mm. - Copy
