Showing 1 - 10 results of 10 for search 'Kjelgaard, Scott O.', query time: 0.06s Refine Results
  1. 1
    Pressure distribution data from tests of 2.29 M (7.5 ft.) span EET high-lift transport aircraft model in the Ames 12-foot pressure tunnel

    Pressure distribution data from tests of 2.29 M (7.5 ft.) span EET high-lift transport aircraft model in the Ames 12-foot pressure tunnel by Kjelgaard, Scott O.

    Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1983
    Format: Government Document Book


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  2. 2
    Pressure distribution data from tests of 2.29 M (7.5 ft.) span EET high-lift transport aircraft model in the Ames 12-foot pressure tunnel

    Pressure distribution data from tests of 2.29 M (7.5 ft.) span EET high-lift transport aircraft model in the Ames 12-foot pressure tunnel by Kjelgaard, Scott O.

    Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1983
    Format: Government Document Book


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  3. 3
    Detailed flow-field measurements over a 75° swept delta wing

    Detailed flow-field measurements over a 75° swept delta wing by Kjelgaard, Scott O.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [National Technical Information Service, distributor], 1990
    Format: Government Document Book


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  4. 4
    Theoretical derivation and calibration technique of a hemispherical-tipped, five-hole probe

    Theoretical derivation and calibration technique of a hemispherical-tipped, five-hole probe by Kjelgaard, Scott O.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1988
    Format: Government Document Book


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  5. 5
    Low-speed tests of a high-aspect-ratio, supercritical-wing transport model equipped with a high-lift flap system in the Langley 4- by 7-meter and Ames 12-foot pressure tunnels

    Low-speed tests of a high-aspect-ratio, supercritical-wing transport model equipped with a high-lift flap system in the Langley 4- by 7-meter and Ames 12-foot pressure tunnels by Morgan, Harry L.

    [Washington, DC] : [Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; National Technical Information Service, distributor], 1983
    Other Authors: “…Kjelgaard, Scott O.…”
    Format: Government Document Book


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  6. 6
    Low-speed tests of a high-aspect-ratio, supercritical-wing transport model equipped with a high-lift flap system in the Langley 4- by 7-meter and Ames 12-foot pressure tunnels

    Low-speed tests of a high-aspect-ratio, supercritical-wing transport model equipped with a high-lift flap system in the Langley 4- by 7-meter and Ames 12-foot pressure tunnels by Morgan, Harry L.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [National Technical Information Service, distributor], 1983
    Other Authors: “…Kjelgaard, Scott O.…”
    Format: Government Document Book


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  7. 7
    An experimental and theoretical investigation of thick wings at various sweep angles in and out of ground effect

    An experimental and theoretical investigation of thick wings at various sweep angles in and out of ground effect by Paulson, John W.

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982
    Other Authors: “…Kjelgaard, Scott O.…”
    Format: Government Document Book


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  8. 8
    Low-speed aerodynamic characteristics of a highly swept, untwisted, uncambered arrow wing

    Low-speed aerodynamic characteristics of a highly swept, untwisted, uncambered arrow wing by Coe, Paul L.

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For the sale by the National Technical Information Service], 1983
    Other Authors: “…Kjelgaard, Scott O.…”
    Format: Government Document Book


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  9. 9
    Detailed near-wake flowfield surveys with comparison to an Euler method of an aspect ratio 4 rectangular wing

    Detailed near-wake flowfield surveys with comparison to an Euler method of an aspect ratio 4 rectangular wing by Klinge, M. D.

    [Washington, D.C.] : [Springfield, Va.] : [National Aeronautics and Space Administration] : [National Technical Information Service, distributor], 1987
    Other Authors: “…Kjelgaard, Scott O.…”
    Format: Government Document Book


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  10. 10
    Detailed near-wake flowfield surveys with comparison to an Euler method of an aspect ratio 4 rectangular wing

    Detailed near-wake flowfield surveys with comparison to an Euler method of an aspect ratio 4 rectangular wing by Klinge, M. D.

    [Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration : National Technical Information Service, distributor, 1987
    Other Authors: “…Kjelgaard, Scott O.…”
    Format: Government Document Book


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