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Supersonic STOVL Research Aircraft

Samuel B. Wilson, George H. Kidwell, G. E. Turney, Al Rogers

Abstract

Two powered-lift concepts, the tandem fan and the longitudinally-arrayed ejector, are integrated with two existing fighter aircraft, the F-l4A and F-16A respectively, to indicate the benefits and/or penalties involved with providing STOVL capability to CTOL aircraft. It is shown that properly designed powered-lift aircraft can achieve either comparable or superior mission performance relative to CTOL aircraft.

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Key concepts: Supersonic speed, Aeronautics, Aerospace engineering, Computer science, Engineering