1973•NASA Technical Reports Server (NASA)Requires access

Subsonic characteristics of a twin-jet swept-wing fighter model with maneuvering devices

Edward John Ray, E. G. Hollingsworth

Abstract

An investigation has been conducted at Mach numbers ranging from 0.06 to 0.94 to determine the effects of various 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.

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Key concepts: Wing, Leading edge, Trailing edge, Camber (aerodynamics), Angle of attack, Wing loading, Wing twist, Chord (peer-to-peer)