Showing 1 - 20 results of 21 for search 'Berrier, Bobby L.', query time: 0.08s Refine Results
  1. 1
    Internal performance of two nozzles utilizing gimbal concepts for thrust vectoring

    Internal performance of two nozzles utilizing gimbal concepts for thrust vectoring by Berrier, Bobby L.

    [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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  2. 2
    Effect of several geometric parameters on the static internal performance of three nonaxisymmetric nozzle concepts

    Effect of several geometric parameters on the static internal performance of three nonaxisymmetric nozzle concepts by Berrier, Bobby L.

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


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  3. 3
    Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft

    Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft by Berrier, Bobby L.

    Washington, D.C. : [Springfield, Va. : For sale by the National Technical Information Service],; Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ;; National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980
    Format: Government Document Book


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  4. 4
    Effect of port corner geometry on the internal performance of a rotating-vane-type thrust reverser

    Effect of port corner geometry on the internal performance of a rotating-vane-type thrust reverser by Berrier, Bobby L.

    [Washington, DC] : [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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  5. 5
    Static internal performance of single-expansion-ramp nozzles with thrust-vectoring capability up to 60°

    Static internal performance of single-expansion-ramp nozzles with thrust-vectoring capability up to 60° by Berrier, Bobby L.

    [Washington, D.C.] : [Springfield, Va.] :; [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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  6. 6
    Effect of port corner geometry on the internal performance of a rotating-vane-type thrust reverser

    Effect of port corner geometry on the internal performance of a rotating-vane-type thrust reverser by Berrier, Bobby L.

    [Washington, DC] : [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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  7. 7
    Static performance of an axisymmetric nozzle with post-exit vanes for multiaxis thrust vectoring

    Static performance of an axisymmetric nozzle with post-exit vanes for multiaxis thrust vectoring by Berrier, Bobby L.

    [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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  8. 8
    Internal performance of two nozzles utilizing gimbal concepts for thrust vectoring

    Internal performance of two nozzles utilizing gimbal concepts for thrust vectoring by Berrier, Bobby L.

    [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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  9. 9
    Static performance of an axisymmetric nozzle with post-exit vanes for multiaxis thrust vectoring

    Static performance of an axisymmetric nozzle with post-exit vanes for multiaxis thrust vectoring by Berrier, Bobby L.

    [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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  10. 10
    Static internal performance of single-expansion-ramp nozzles with thrust-vectoring capability up to 60⁰

    Static internal performance of single-expansion-ramp nozzles with thrust-vectoring capability up to 60⁰ by Berrier, Bobby L.

    [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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  11. 11
    Investigation of installation effects on single-engine convergent-divergent nozzles

    Investigation of installation effects on single-engine convergent-divergent nozzles by Burley, James R.

    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: “…Berrier, Bobby L.…”
    Format: Government Document Book


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  12. 12
    Static internal performance of single expansion-ramp nozzles with thrust vectoring and reversing

    Static internal performance of single expansion-ramp nozzles with thrust vectoring and reversing by Re, Richard 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
    Other Authors: “…Berrier, Bobby L.…”
    Format: Government Document Book


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  13. 13
    Static performance of nonaxisymmetric nozzles with yaw thrust-vectoring vanes

    Static performance of nonaxisymmetric nozzles with yaw thrust-vectoring vanes by Mason, Mary L.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1988
    Other Authors: “…Berrier, Bobby L.…”
    Format: Government Document Book


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  14. 14
    Effects of tail span and empennage arrangement on drag of a typical single-engine fighter aft end

    Effects of tail span and empennage arrangement on drag of a typical single-engine fighter aft end by Burley, James R.

    [Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1984
    Other Authors: “…Berrier, Bobby L.…”
    Format: Government Document Book


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  15. 15
    Effects of tail span and empennage arrangement on drag of a typical single-engine fighter aft end

    Effects of tail span and empennage arrangement on drag of a typical single-engine fighter aft end by Burley, James R.

    [Washington, D.C.] : [Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; For sale by the National Technical Information Service], 1984
    Other Authors: “…Berrier, Bobby L.…”
    Format: Government Document Book


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  16. 16
    Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane

    Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane by Reubush, David E.

    [Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1987
    Other Authors: “…Berrier, Bobby L.…”
    Format: Government Document Book


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  17. 17
    Investigation of axisymmetric and nonaxisymmetric nozzels installed on a 0.10-scale F-18 protype airplane model

    Investigation of axisymmetric and nonaxisymmetric nozzels installed on a 0.10-scale F-18 protype airplane model by Capone, Francis J.

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1980
    Other Authors: “…Berrier, Bobby L.…”
    Format: Government Document Book


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  18. 18
    Static performance of nonaxisymmetric nozzles with yaw thrust-vectoring vanes

    Static performance of nonaxisymmetric nozzles with yaw thrust-vectoring vanes by Mason, Mary L.

    [Washington, DC] : [Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; For sale by the National Technical Information Service], 1988
    Other Authors: “…Berrier, Bobby L.…”
    Format: Government Document Book


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  19. 19
    Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane

    Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane by Reubush, David E.

    [Washington, D.C.] : [Springfield,Va. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; For sale by the National Technical Information Service], 1987
    Other Authors: “…Berrier, Bobby L.…”
    Format: Government Document Book


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  20. 20
    Investigation of installation effects on twin-engine convergent-divergent nozzles

    Investigation of installation effects on twin-engine convergent-divergent nozzles by Bare, E. Ann

    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: “…Berrier, Bobby L.…”
    Format: Government Document Book


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