An investigation has been conducted at Mach numbers ranging from 0.06 to 0.94 to determine ous combinations of leading-edge slat devices on the static aerodynamic characteristics of a twin-jet swept-wing fighter model. The study also included a determination of the effects of wing leading-edge droop, trailing-edge chord-extensions, wing fences, and wing-planform and camber modifications. The angle-of-attack range generally extended from about minus 2 deg to 24 deg and the sideslip angles ranged from about minus 6 deg to 13 deg. (Author)
Subsonic Characteristics of a Twin-Jet Swept-Wing Fighter Model with Maneuvering Devices
1973
292 pages
Report
No indication
English