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Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds

Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds - - Washington, D.C. National Aeronautics and Space Admin 1987 - 124 p. - NASA TP 2588 : 1987 .

ISBN:

Subjects--Topical Terms:

Nozzle-afterbody flow interactions, Reynolds number effects, Wind tunnel and flight comparison

Universal Decimal Class. No.: LNASA TP 2588 : 1987

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