Showing 1 - 20 results of 27 for search 'Mineck, Raymond E.', query time: 0.08s Refine Results
  1. 1
    Aerodynamic characteristics of a 1/6-scale powered model of the rotor systems research aircraft

    Aerodynamic characteristics of a 1/6-scale powered model of the rotor systems research aircraft by Mineck, Raymond E.

    Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1977
    Format: Government Document Book


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  2. 2
    High Reynolds number tests of the NASA SC(2)-0012 airfoil in the Langley 0.3-meter transonic cryogenic tunnel

    High Reynolds number tests of the NASA SC(2)-0012 airfoil in the Langley 0.3-meter transonic cryogenic tunnel by Mineck, Raymond E.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1987
    Format: Government Document Book


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  3. 3
    Application of two procedures for dual-point design of transonic airfoils

    Application of two procedures for dual-point design of transonic airfoils by Mineck, Raymond E.

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1994
    Format: Government Document Book


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  4. 4
    Comparison of a two-dimensional adaptive-wall technique with analytical wall interference correction techniques

    Comparison of a two-dimensional adaptive-wall technique with analytical wall interference correction techniques by Mineck, Raymond E.

    [Washington, DC] : [Springfield, Va. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; For sale by the National Technical Information Service], 1992
    Format: Government Document Book


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  5. 5
    Reynolds number effects on the performance of lateral control devices

    Reynolds number effects on the performance of lateral control devices by Mineck, Raymond E.

    Hampton, Va. : Springfield, Va. :; Hampton, Va. : Springfield, VA : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor, 2000
    Format: Government Document Book


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  6. 6
    Wind-tunnel investigation of aerodynamic efficiency of three planar ellipyical wings with curvature of quarter-chord line

    Wind-tunnel investigation of aerodynamic efficiency of three planar ellipyical wings with curvature of quarter-chord line by Mineck, Raymond E.

    [Washington, DC] : [Springfield, Va. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; National Technical Information Service, distributor], 1993
    Format: Government Document Book


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  7. 7
    Assessment of potential aerodynamic benefits from spanwise blowing at the wingtip

    Assessment of potential aerodynamic benefits from spanwise blowing at the wingtip by Mineck, Raymond E.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1992
    Format: Government Document Book


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  8. 8
    Hardware and operating features of the adaptive wall test section for the Langley 0.3-meter transonic cryogenic tunnel

    Hardware and operating features of the adaptive wall test section for the Langley 0.3-meter transonic cryogenic tunnel by Mineck, Raymond E.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1989
    Format: Government Document Book


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  9. 9
    Comparison of a two-dimensional adaptive-wall technique with analytical wall interference correction techniques

    Comparison of a two-dimensional adaptive-wall technique with analytical wall interference correction techniques by Mineck, Raymond E.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [For sale by the National Technical Information Service], 1992
    Format: Government Document Book


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  10. 10
    Effect of rotor wake on aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft

    Effect of rotor wake on aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft by Mineck, Raymond E.

    Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1977
    Format: Government Document Book


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  11. 11
    Wind-tunnel investigation of aerodynamic efficiency of three planar ellipyical wings with curvature of quarter-chord line

    Wind-tunnel investigation of aerodynamic efficiency of three planar ellipyical wings with curvature of quarter-chord line by Mineck, Raymond E.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1993
    Format: Government Document Book


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  12. 12
    Wall interference tests of a CAST 10-2/DOA 2 airfoil in an adaptive-wall test section

    Wall interference tests of a CAST 10-2/DOA 2 airfoil in an adaptive-wall test section by Mineck, Raymond E.

    [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1987
    Format: Government Document Book


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  13. 13
    Wall interference tests of a CAST 10-2/DOA 2 airfoil in an adaptive-wall test section

    Wall interference tests of a CAST 10-2/DOA 2 airfoil in an adaptive-wall test section by Mineck, Raymond E.

    [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1987
    Format: Government Document Book


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  14. 14
    Calibration of the 13- by 13-inch adaptive wall test section for the Langley 0.3-Meter Transonic Cryogenic Tunnel

    Calibration of the 13- by 13-inch adaptive wall test section for the Langley 0.3-Meter Transonic Cryogenic Tunnel by Mineck, Raymond E.

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


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  15. 15
    High Reynolds number tests of the NASA SC(2)-0012 airfoil in the Langley 0.3-meter transonic cryogenic tunnel

    High Reynolds number tests of the NASA SC(2)-0012 airfoil in the Langley 0.3-meter transonic cryogenic tunnel by Mineck, Raymond E.

    [Washington, DC] : [Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service], 1987
    Format: Government Document Book


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  16. 16
    Calibration of the 13- by 13-inch adaptive wall test section for the Langley 0.3-Meter Transonic Cryogenic Tunnel

    Calibration of the 13- by 13-inch adaptive wall test section for the Langley 0.3-Meter Transonic Cryogenic Tunnel by Mineck, Raymond E.

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


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  17. 17
    Tail contribution to the directional aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft with a tail rotor

    Tail contribution to the directional aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft with a tail rotor by Mineck, Raymond E.

    Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1977
    Format: Government Document Book


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  18. 18
    Study of potential aerodynamic benefits from spanwise blowing at wingtip

    Study of potential aerodynamic benefits from spanwise blowing at wingtip by Mineck, Raymond E.

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  19. 19
    Computer model to simulate testing at the National Transonic Facility

    Computer model to simulate testing at the National Transonic Facility

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1995
    Other Authors: “…Mineck, Raymond E.…”
    Format: Government Document Book


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  20. 20
    Adaptive wind tunnel walls a selected, annotated bibliography

    Adaptive wind tunnel walls a selected, annotated bibliography by Tuttle, Marie H.

    [Washington, DC] : [Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; For sale by the National Technical Information Service], 1986
    Other Authors: “…Mineck, Raymond E.…”
    Format: Government Document Book


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