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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 Rudder.
AguilarAlex created this project
almost 6 years ago
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 Rudder.
by simscalesimscale