Search results for: Berrier, Bobby L.

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  1. 1

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

    Authors: Berrier, Bobby L.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; 1980
    Physical Description: 215 pages : chiefly illustrations ; 27 cm.
    Government Document Microfilm Book
  2. 2

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

    Authors: Berrier, Bobby L.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1979
    Physical Description: 134 pages : illustrations ; 27 cm.
    Government Document Book
  3. 3

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

    Authors: Berrier, Bobby L.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1986
    Physical Description: 1 volume.
    Government Document Microfilm Book
  4. 4

    Static internal performance of single-expansion-ramp nozzles with thrust-vectoring capability up to 60.

    Authors: Berrier, Bobby L.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1984
    Physical Description: 1 volume.
    Government Document Microfilm Book
  5. 5

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

    Authors: Berrier, Bobby L.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1988
    Physical Description: 1 volume.
    Government Document Microfilm Book
  6. 6

    Internal performance of two nozzles utilizing gimbal concepts for thrust vectoring

    Authors: Berrier, Bobby L.
    Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1990
    Physical Description: 1 volume.
    Government Document Microfilm Book
  7. 7

    Operating characteristics of the multiple critical venturi system and secondary calibration nozzles used for weight-flow measurements in the Langley 16-foot transonic tunnel

    Authors: Berrier, Bobby L.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985
    Physical Description: 1 volume., Also available via Internet from the NTRS web site. Address as of 07/07/08: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19860000549%5F1986000549.pdf ; current access is available via PURL.
    Connect to online resource - All users (Federal Depository Library Program Persistant URL)
    Government Document Microfilm Book
  8. 8

    High Reynolds number investigation of a flush-mounted, S-duct inlet with large amounts of boundary layer ingestion

    Authors: Berrier, Bobby L.
    Published: National Aeronautics and Space Administration, Langley Research Center, 2005
    Physical Description: 1 online resource (165 pages) : illustrations (some color).
    Connect to online resource - All users (Federal Depository Library Program Persistant URL)
    Government Document Electronic eBook
  9. 9

    Effect of plug and shroud geometry variables on plug-nozzle performance at transonic speeds

    Authors: Berrier, Bobby L.
    Published: National Aeronautics and Space Administration, 1969
    Physical Description: 1 online resource (195 pages) : illustrations.
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    Government Document Electronic eBook
  10. 10

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

    Authors: Berrier, Bobby L., Re, Richard J.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980
    Physical Description: 1 online resource (215 pages) : chiefly illustrations.
    Connect to online resource - All users (Federal Depository Library Program Persistant URL)
    Government Document Electronic eBook
  11. 11

    Static internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to 60°

    Authors: Berrier, Bobby L., Leavitt, Laurence D.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1984
    Physical Description: 1 online resource (141 pages) : illustrations.
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    Government Document Electronic eBook
  12. 12

    Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles

    Authors: Mason, Mary L., Berrier, Bobby L.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985
    Physical Description: 1 online resource (216 pages) : illustrations.
    Connect to online resource - All users (Federal Depository Library Program Persistant URL)
    Government Document Electronic eBook
  13. 13

    Transonic aerodynamic characteristics of powered models of several Apollo launch-escape vehicle configurations

    Authors: Berrier, Bobby L., Pendergraft, Odis C.
    Published: National Aeronautics and Space Administration, Langley Research Center, 1968
    Physical Description: 1 online resource (41 pages, 1 unnumbered page) : illustrations.
    Connect to online resource - All users (Federal Depository Library Program Persistant URL)
    Government Document Electronic eBook
  14. 14

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

    Authors: Re, Richard J.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982
    Other Authors: “…Berrier, Bobby L.…”
    Physical Description: 140 pages : illustrations ; 28 cm.
    Government Document Book
  15. 15

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

    Authors: Capone, Francis J.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1980
    Other Authors: “…Berrier, Bobby L.…”
    Physical Description: 301 pages : illustrations ; 28 cm.
    Government Document Book
  16. 16

    Static performance of nonaxisymmetric nozzles with yaw thrust-vectoring vanes

    Authors: Mason, Mary L.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1988
    Other Authors: “…Berrier, Bobby L.…”
    Physical Description: 1 volume.
    Government Document Microfilm Book
  17. 17

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

    Authors: Burley, James R.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1984
    Other Authors: “…Berrier, Bobby L.…”
    Physical Description: 1 volume.
    Government Document Microfilm Book
  18. 18

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

    Authors: Reubush, David E.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1987
    Other Authors: “…Berrier, Bobby L.…”
    Physical Description: 1 volume.
    Government Document Microfilm Book
  19. 19

    Investigation of installation effects on single-engine convergent-divergent nozzles

    Authors: Burley, James R.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982
    Other Authors: “…Berrier, Bobby L.…”
    Physical Description: 231 pages : illustrations ; 28 cm.
    Government Document Book
  20. 20

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

    Authors: Bare, E. Ann
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1983
    Other Authors: “…Berrier, Bobby L.…”
    Physical Description: 188 pages : illustrations ; 28 cm.
    Government Document Book