Summary Technical Report Variable Camber Wing - Phase I
Summary Technical Report Variable Camber Wing - Phase I
- Neue Suche nach: D. K. Gould
- Neue Suche nach: D. K. Gould
A variable camber wing system has been designed for high performance fighter and attack airplanes. This system combines aerodynamic improvements resulting from advanced technology wing shapes and smoothly contoured leading and trailing edge flaps with an automatic flight control system that deploys the flaps in response to airplane flight requirements. This system achieves outstanding transonic combat and low speed performance without degrading supersonic capability. (Author)
Dokumentinformationen
Summary Technical Report Variable Camber Wing - Phase I
1973
73 pages
Report
Keine Angabe
Englisch
Aircraft , Fluid Mechanics , Variable incidence wings , Jet fighters , Wings , Leading edge flaps , Camber , Variations , Leading edges , Trailing edge , Flight control systems , Transonic flight , Supersonic flight , Performance(Engineering) , Low velocity , Handling , Airfoils , Flaps(Control surfaces) , Attack aircraft , Flight loads , Structural properties , Skin(General) , Fiberglass , Laminates , Flexible materials , Flexible structures , Variable camber wings , Advanced technology variable camber , Design , F-8 aircraft , ATVCW(Advanced technology variable camber)
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