A variable camber wing system has been designed for high performance fighter and attack airplanes. Analysis derived from theory and wind tunnel test data indicates that variable camber provides substantial improvements in combat capability over existing airplanes. The variable camber system consists of: (1) An advanced aerodynamic technology wing design; (2) A practical mechanism that varies the camber of the advanced technology wing. This camber varying mechanism is unique in that a flexible skin panel is used to provide smooth, continuous (conformal) curved upper surface contours; (3) A flight control system which automatically produces the leading and trailing contours producing the maximum performance advantages; (4) A manual mode which provides a high lift and drag landing configuration; (5) A redundancy level for each of the system elements to provide safe operation; (6) and A design which features battle damage resistant features. (Author)
Mechanization and Utilization of Variable Camber in Fighter and Attack Airplanes
1973
94 pages
Report
Keine Angabe
Englisch
Aircraft , Camber , Jet fighters , Attack bombers , Control systems , Aerodynamic control surfaces , Trailing edge , Leading edges , Deflection , Actuators , Flight paths , Maneuverability , Aerial warfare , Mission profiles , Acceleration , Turning flight , Range(Distance) , Lift , Drag , Patents , Advanced technology variable camber wings , Atvcw(Advanced technology variable camber wing)
Results of power systems study advanced fighter/attack and V/STOL airplanes
Tema Archiv | 1979
|Evaluation of Agility Metrics for Fighter Airplanes
Online Contents | 1997
Emergency measures for increasing range of fighter airplanes
Engineering Index Backfile | 1943
|SOME HIGH SPEED EXPERIENCE WITH FIGHTER TYPE AIRPLANES
SAE Technical Papers | 1950
|