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139
3
2 Geometries
1 Mesh
0 Simulation setups
0 ResultsProject Goal : To Investigate the the Optimal Aerodynamics Efficiency for a Given Flight Attitude Secenario(s). Simulation Type: Incompressible-Instability Transient Flow Detail(s):
2 Geometries 1 Mesh 0 Simulation setups 0 ResultsProject Goal : To Investigate the the Optimal Aerodynamics Efficiency for a Given Flight Attitude Secenario(s). Simulation Type: Incompressible-Instability Transient Flow Detail(s):
by simscalesimscale
simscale created this project
about 6 years ago
baswam95 copied this project
over 5 years ago
