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Numerical analysis of rapid, high angle of attack manoeuvres

Goetzendorf-Grabowski T.

Research Bulletin / Warsaw University of Technology, Institute of Aeronautics and Applied Mechanics

1998

nr 8

199-204

This paper presents numerical analysis of rapid, high angle of attack manoeuvres. The physical and mathematical models of an aircraft motion were shown. Paper contains selected results of the following manoeuvres: - water bomb dropping from the fire fighting aircraft PZL-106 Kruk, - theoretically predicted Cobra manoeuvre for the jet combat aircraft Skorpion (project developed in PZL-Okęcie). Calculations for Cobra manoeuvre were performed in the extended range of the angle of attack (from 0° to 90°).