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Glider BA: Left Aileron
235
0Statistics
18 Geometries
8 Meshes
9 Simulation setups
9 Results
18 Geometries 8 Meshes 9 Simulation setups 9 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 Left Aileron.
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AguilarAlex created this project