Set up your own cloud-native simulation in minutes.Start Simulating Now
Glider BA: Left Aileron
242
0
Statistics
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.
Related Projects
Project History
AguilarAlex created this project