Showing 1 - 15 results of 15 for search 'Mann, Michael J.', query time: 0.08s Refine Results
  1. 1
    Aerodynamic design for improved maneuverability by use of three-dimensional transonic theory

    Aerodynamic design for improved maneuverability by use of three-dimensional transonic theory by Mann, Michael J.

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1984
    Format: Government Document Book


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  2. 2
    Forward-swept-wing configuration designed for high maneuverability by use of a transonic computational method

    Forward-swept-wing configuration designed for high maneuverability by use of a transonic computational method by Mann, Michael J.

    [Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1986
    Format: Government Document Book


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  3. 3
    Subsonic longitudinal and lateral-directional characteristics of a forward-swept-wing fighter configuration at angles of attack up to 47⁰

    Subsonic longitudinal and lateral-directional characteristics of a forward-swept-wing fighter configuration at angles of attack up to 47⁰ by Mann, Michael J.

    [Washington, D.C.] : [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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  4. 4
    Design of supersonic transport flap systems for thrust recovery at subsonic speeds

    Design of supersonic transport flap systems for thrust recovery at subsonic speeds by Mann, Michael J.

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1999
    Format: Government Document Book


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  5. 5
    Supercritical maneuvering fighter configuration : wind-tunnel investigation at Mach numbers of 0.60 to 0.95

    Supercritical maneuvering fighter configuration : wind-tunnel investigation at Mach numbers of 0.60 to 0.95 by Mann, Michael J.

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982
    Format: Government Document Book


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  6. 6
    The design of supercritical wings by the use of three-dimensional transonic theory

    The design of supercritical wings by the use of three-dimensional transonic theory by Mann, Michael J.

    [Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1979
    Format: Government Document Book


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  7. 7
    Forward-swept-wing configuration designed for high maneuverability by use of a transonic computational method

    Forward-swept-wing configuration designed for high maneuverability by use of a transonic computational method by Mann, Michael J.

    [Washington, D.C.] : [Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; For sale by the National Technical Information Service], 1986
    Format: Government Document Book


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  8. 8
    Subsonic longitudinal and lateral-directional characteristics of a forward-swept-wing fighter configuration at angles of attack up to 47°

    Subsonic longitudinal and lateral-directional characteristics of a forward-swept-wing fighter configuration at angles of attack up to 47° by Mann, Michael J.

    [Washington, D.C.] : [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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  9. 9
    Transonic aerodynamic characteristics of a supercritical-wing transport model with trailing-edge controls

    Transonic aerodynamic characteristics of a supercritical-wing transport model with trailing-edge controls by Mann, Michael J., Langhans, Richard A.

    Washington : Springfield, Va. :; 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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  10. 10
    Survey and analysis of research on supersonic drag-due-to-lift minimumization with recommendations for wing design

    Survey and analysis of research on supersonic drag-due-to-lift minimumization with recommendations for wing design by Carlson, Harry W.

    [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
    Other Authors: “…Mann, Michael J.…”
    Format: Government Document Book


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  11. 11
    Theoretical estimation of the transonic aerodynamic characteristics of a supercritical-wing transport model with trailing-edge controls

    Theoretical estimation of the transonic aerodynamic characteristics of a supercritical-wing transport model with trailing-edge controls by Luckring, James M.

    [Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978
    Other Authors: “…Mann, Michael J.…”
    Format: Government Document Book


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  12. 12
    Survey and analysis of research on supersonic drag-due-to-lift minimumization with recommendations for wing design

    Survey and analysis of research on supersonic drag-due-to-lift minimumization with recommendations for wing design by Carlson, Harry W.

    [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
    Other Authors: “…Mann, Michael J.…”
    Format: Government Document Book


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  13. 13
    Experimental study of wing leading-edge devices for improved maneuver performance of a supercritical maneuvering fighter configuration

    Experimental study of wing leading-edge devices for improved maneuver performance of a supercritical maneuvering fighter configuration

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


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  14. 14
    Validation of a computer code for analysis of subsonic aerodynamic performance of wings with flaps in combination with a canard or horizontal tail and an application of optimization

    Validation of a computer code for analysis of subsonic aerodynamic performance of wings with flaps in combination with a canard or horizontal tail and an application of optimizatio... by Carlson, Harry W.

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


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  15. 15
    Validation of a computer code for analysis of subsonic aerodynamic performance of wings with flaps in combination with a canard or horizontal tail and an application of optimization

    Validation of a computer code for analysis of subsonic aerodynamic performance of wings with flaps in combination with a canard or horizontal tail and an application of optimizatio... by Carlson, Harry W.

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


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