The primary objective is to determine how an airplane configuration should be modeled to predict both longitudinal and lateral aerodynamic characteristics at high angles of attack. A generic fighter model, an F-16 and an F-18 configuration with leading edge flap deflection and an F-106B configuration were investigated. Furthermore, the F-16XL and X-29 configurations were examined. Some calculated results are given.
Calculation of aerodynamic characteristics at high angles of attack for airplane configurations
1987-02-24
Report
No indication
English
Unsteady aerodynamic modeling and identification of airplane at high angles of attack
British Library Online Contents | 1996
|Aerodynamic characteristics at high angles of attack
NTRS | 1977
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