A six degree of freedom flight simulation model was developed for digital computers to investigate the response of aircraft to a pair of trailing vortices. The model was used to simulate the flight of a light, two-seat training aircraft and a twin-engined commercial transport into the vortices shed by medium weight and heavy weight aircraft. (Author)
A Dynamic Analysis of Aeroplanes Encountering Vortex Wake Turbulence
1973
52 pages
Report
Keine Angabe
Englisch
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