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  • Other Sources  (2)
  • AIRCRAFT  (2)
  • Aeronautics (General)
  • 1970-1974  (2)
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  • Other Sources  (2)
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  • 1
    Publication Date: 2019-06-27
    Description: The changes in thrust minus drag performance as well as longitudinal and directional stability and control characteristics of a single-engine jet aircraft attributable to an in-flight thrust reverser of the blocker-deflector door type were investigated in a 16-foot transonic wind tunnel. The longitudinal and directional stability data are presented. Test conditions simulated landing approach conditions as well as high speed maneuvering such as may be required for combat or steep descent from high altitude.
    Keywords: AIRCRAFT
    Type: NASA-TN-D-6886 , L-8395
    Format: application/pdf
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  • 2
    Publication Date: 2019-06-27
    Description: A wind-tunnel investigation has been conducted to determine the exhaust-nozzle aerodynamic and propulsive characteristics for a twin-jet variable-wing-sweep fighter airplane model. The powered model was tested in the Langley 16-foot transonic tunnel and in the Langley 4-foot supersonic pressure tunnel at Mach numbers to 2.2 and at angles of attack from about minus 2 to 6 deg. Compressed air was used to simulate the nozzle exhaust flow at values of jet total-pressure ratio from approximately 1 (jet off) to about 21. Effects of configuration variables such as speed-brake deflection, store installation, and boundary-layer thickness on the the nozzle characteristics were also investigated.
    Keywords: AIRCRAFT
    Type: NASA-TM-X-2947 , L-9273
    Format: application/pdf
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