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Glider BA: Body/Fuselage
230
0Statistics
5 Geometries
0 Meshes
2 Simulation setups
2 Results
5 Geometries 0 Meshes 2 Simulation setups 2 ResultsAbout this project
For a bachelor thesis, the coefficients of drag, lift and pitching moment need to be calculated. Model is a RC Glider. Here is the simulation for the Fuselage.
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AguilarAlex created this project