Studies of generic aircraft configurations to determine the payoff of thrust vectoring for direct lift during STOL landings and takeoff and for control power augmentation during weapons-delivery maneuvers are described. Results show that for a nominal 1000-foot landing distance, direct-lift benefits are small, but significant improvements in control power augmentation contribute to payoffs in takeoff distance and recovery from roll-pitch-coupling-induced departures at high angles of attack.
Application of thrust vectoring for STOL
V/STOL Conference ; 1981 ; Palo Alto, CA
1981-12-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Application of thrust vectoring for STOL
AIAA | 1981
|Development of Thrust Deflection and Vectoring - V/STOL
SAE Technical Papers | 1966
|