Set up your own cloud-native simulation in minutes.Start Simulating Now
Glider BA: Body/Fuselage
233
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.
Related Projects
Project History
AguilarAlex created this project