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Drone-FlowAnalysis
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2 Geometries
1 Mesh
0 Simulation setups
0 Results
2 Geometries 1 Mesh 0 Simulation setups 0 ResultsAbout this project
Project Goal : To Investigate the the Optimal Aerodynamics Efficiency for a Given Flight Attitude Secenario(s). Simulation Type: Incompressible-Instability Transient Flow Detail(s):
