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Supersonic STOVL research aircraftTwo powered-lift concepts, the tandem fan and the longitudinally-arrayed ejector, are integrated with two existing fighter aircraft, the F-14A 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.
Document ID
19830056747
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wilson, S. B., III (NASA Ames Research Center Moffett Field, CA, United States)
Kidwell, G. H., Jr. (NASA Ames Research Center Moffett Field, CA, United States)
Turney, G. E. (NASA Lewis Research Center Cleveland, OH, United States)
Rogers, A. (Grumman Aerospace Corp. El Segundo, CA, United States)
Date Acquired
August 11, 2013
Publication Date
October 1, 1982
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
SAE PAPER 821375
Report Number: SAE PAPER 821375
Accession Number
83A37965
Distribution Limits
Public
Copyright
Other

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