The main peculiarities of aerodynamic design of highly maneuverable aircraft are examined. The possibilities of improving the aerodynamic characteristics of aircraft at high angles of attack by use of high-lift devices and powered-lift systems (boundary layer control, blowing over wing, engine thrust vectoring) are shown. The conditions of controllable maneuver at high post-stalled angles of attack (alpha is less than or equal to 90 degrees) are established. Results of experimental investigations on the influence of wing planform and locations of aircraft components (wing, empennage) on the longitudinal stability and controllability at high angles of attack are presented. A comparative analysis of aerodynamic and maneuver performance of aircraft of various configurations (conventional, three-surface, canard) is performed.
Aerodynamic Design of Super Maneuverable Aircraft
1994
6 pages
Report
No indication
English
Aircraft , Aerodynamics , Aerodynamic characteristics , Aircraft design , Boundary layer control , Canard configurations , Highly maneuverable aircraft , Maneuverability , Thrust vector control , Angle of attack , Longitudinal stability , Tail assemblies , Wing planforms , Blowing , Controllability , Foreign technology
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