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  1. 1
    F-15 rotary balance data for an angle-of-attack range of 8° to 90° /

    F-15 rotary balance data for an angle-of-attack range of 8° to 90° / by Barnhart, Billy

    Published 1982
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  2. 2
    Fastener load tests and retention systems tests for cryogenic wind-tunnel models /

    Fastener load tests and retention systems tests for cryogenic wind-tunnel models / by Wallace, John W.

    Published 1984
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  3. 3
    Wind-tunnel/flight correlation, 1981 : proceedings of a miniworkshop held at NASA Langley Research Center, Hampton, Virginia, November 19-20, 1981 /

    Wind-tunnel/flight correlation, 1981 : proceedings of a miniworkshop held at NASA Langley Research Center, Hampton, Virginia, November 19-20, 1981 /

    Published 1981
    “…National Aeronautics and Space Administration, Scientific …”
    Government Document Conference Proceeding Book
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  4. 4
    Design study of test models of maneuvering aircraft configurations for the National Transonic Facility /

    Design study of test models of maneuvering aircraft configurations for the National Transonic Facility /

    Published 1984
    “…National Aeronautics and Space Administration, Scientific …”
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  5. 5
    Flight and wind-tunnel comparisons of the inlet/airframe interaction of the F-15 airplane /

    Flight and wind-tunnel comparisons of the inlet/airframe interaction of the F-15 airplane / by Webb, Lannie D.

    Published 1984
    “…National Aeronautics and Space Administration, Scientific …”
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  6. 6
    Evaluation of the Langley 4- by 7-meter tunnel for propeller noise measurements /

    Evaluation of the Langley 4- by 7-meter tunnel for propeller noise measurements / by Block, P. J. W.

    Published 1984
    “…National Aeronautics and Space Administration, Scientific …”
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  7. 7
    Effect of jet exit vanes on flow pulsations in an open-jet wind tunnel

    Effect of jet exit vanes on flow pulsations in an open-jet wind tunnel

    Published 1985
    “…National Aeronautics and Space Administration, Scientific …”
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  8. 8
    Effects of cortex flaps on the low-speed aerodynamic characteristics of an arrow wing /

    Effects of cortex flaps on the low-speed aerodynamic characteristics of an arrow wing / by Yip, Long P.

    Published 1981
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  9. 9
    Rotary balance data for an F-15 model with fuel tanks for an angle-of-attack range of 8° to 90° /

    Rotary balance data for an F-15 model with fuel tanks for an angle-of-attack range of 8° to 90° / by Barnhart, Billy

    Published 1982
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  10. 10
    Loads and performance data from a wind-tunnel test of model articulated helicopter rotors with two different blade torsional stiffnesses /

    Loads and performance data from a wind-tunnel test of model articulated helicopter rotors with two different blade torsional stiffnesses / by Yeager, William T.

    Published 1983
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  11. 11
    Finite-rate water condensation in combustion-heated wind tunnels

    Finite-rate water condensation in combustion-heated wind tunnels by Erickson, Wayne D. (Wayne Douglas), 1932-

    Published 1988
    “…National Aeronautics and Space Administration, Scientific …”
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    Government Document Microfilm Book
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  12. 12
    Flow visualization and laser velocimetry for wind tunnels : proceedings of a NASA workshop held at Langley Research Center, Hampton, Virginia, March 25-26, 1982 /

    Flow visualization and laser velocimetry for wind tunnels : proceedings of a NASA workshop held at Langley Research Center, Hampton, Virginia, March 25-26, 1982 /

    Published 1982
    “…National Aeronautics and Space Administration, Scientific …”
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  13. 13
    Improvement in the quality of flow visualization in the Langley 0.3-meter transonic cryogenic tunnel

    Improvement in the quality of flow visualization in the Langley 0.3-meter transonic cryogenic tunnel by Snow, W. L.

    Published 1986
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  14. 14
    Vapor-screen technique for flow visualization in the Langley Unitary Plan Wind Tunnel

    Vapor-screen technique for flow visualization in the Langley Unitary Plan Wind Tunnel

    Published 1985
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  15. 15
    Study on needs for a magnetic suspension system operating with a transonic wind tunnel

    Study on needs for a magnetic suspension system operating with a transonic wind tunnel by Martindale, W. R.

    Published 1985
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  16. 16
    Experimental evaluation of two turning vane designs for fan drive corner 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel

    Experimental evaluation of two turning vane designs for fan drive corner 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel by Boldman, Donald R.

    Published 1987
    “…National Aeronautics and Space Administration, Scientific …”
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  17. 17
    Experimental evaluation of blockage ratio and plenum evacuation system flow effects on pressure distribution for bodies of revolution in 0.1-scale model test section of NASA Lewis Research Center's proposed altitude wind tunnel

    Experimental evaluation of blockage ratio and plenum evacuation system flow effects on pressure distribution for bodies of revolution in 0.1-scale model test section of NASA Lewis... by Burley, Richard R.

    Published 1987
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  18. 18
    Wind-tunnel/flight correlation study of aerodynamic characteristics of a large flexible supersonic cruise airplane (XB-70-1)

    Wind-tunnel/flight correlation study of aerodynamic characteristics of a large flexible supersonic cruise airplane (XB-70-1)

    Published 1979
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  19. 19
    Pressure data for four analytically defined arrow wings in supersonic flow /

    Pressure data for four analytically defined arrow wings in supersonic flow / by Townsend, James C. (James Courtland), 1938-

    Published 1980
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  20. 20
    Wind-tunnel test of an articulated helicopter rotor model with several tip shapes /

    Wind-tunnel test of an articulated helicopter rotor model with several tip shapes / by Berry, John D.

    Published 1980
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