The document presents preliminary drawings and layouts of an advanced technology wing with variable camber leading and trailing edge systems for an F-8 flight demonstrator airplane. Short descriptions accompany drawings of the wing structural arrangement, four leading edge variable camber concepts, and a trailing edge variable camber concept. In addition, the wing control surface actuation system arrangement is shown with a schematic of the hydraulic system. (Author)
Preliminary Drawings and Layouts Variable Camber Wing - Phase I
1973
32 pages
Report
Keine Angabe
Englisch
Aircraft , Fluid Mechanics , Wings , Jet fighters , Variable incidence wings , Leading edge flaps , Camber , Leading edges , Trailing edge , Skin(General) , Performance(Engineering) , Loads(Forces) , Structures , Stresses , Safety , Weight , Strength , Geometry , Hydraulic actuators , Ailerons , Flight control systems , Pitch , Variable camber wings , Advanced technology variable camber wing , F-8 aircraft , ATVCW(Advanced technology variable camber wing)
NTIS | 1973
NTIS | 1973
NTIS | 1973
Additional Studies, Variable Camber Wing - Phase I
NTIS | 1974
|Variable Camber Compliant Wing - Design
AIAA | 2015
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