The AD-1 is a variable-sweep oblique-wing research airplane that exhibits unconventional stability and control characteristics. In this report, flight-determined and predicted stability and control derivatives for the AD-1 airplane are compared. The predictions are based on both wind tunnel and computational results. A final best estimate of derivatives is presented.
Flight-Determined Aerodynamic Derivatives of the AD-1 Oblique-Wing Research Airplane
1984
39 pages
Report
No indication
English