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Case Studies

University of Kansas

Students at the University of Kansas are using AAA to develop a dynamic model of a goose in flight. The aerodynamic characteristics and the stability & control parameters per time step are calculated over the wing flapping motion and used to generate a dynamic model.

Aeronautical Engineering

At 0 second time interval

Aeronautical Engineering Ross_Goose_t=0.095

At 0.095 seconds time interval

Aeronautical Engineering Ross_Goose_t=0.14

At 0.14 seconds time interval

Aeronautical Engineering Ross_Goose_t=0.18

At 0.18 seconds time interval

Aeronautical Engineering Ross_Goose_t=0.245

At 0.245 seconds time interval