Showing 1 - 20 results of 36 for search 'Berrier, Bobby L.', query time: 0.32s Refine Results
  1. 1
    High Reynolds number investigation of a flush-mounted, S-duct inlet with large amounts of boundary layer ingestion /
    by Berrier, Bobby L, Berrier, Bobby L
    Published 2005

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  2. 2
    Operating characteristics of the multiple critical venturi system and secondary calibration nozzles used for weight-flow measurements in the Langley 16-foot transonic tunnel /
    by Berrier, Bobby L, Berrier, Bobby L
    Published 1985

    Government Document Book
  3. 3
    Effect of several geometric parameters on the static internal performance of three nonaxisymmetric nozzle concepts /
    by Berrier, Bobby L
    Published 1979

    Government Document Book
  4. 4
    Effect of plug and shroud geometry variables on plug-nozzle performance at transonic speeds /
    by Berrier, Bobby L.
    Published 1969

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  5. 5
    Static performance of an axisymmetric nozzle with post-exit vanes for multiaxis thrust vectoring
    by Berrier, Bobby L
    Published 1988

    Government Document Book
  6. 6
    Effect of port corner geometry on the internal performance of a rotating-vane-type thrust reverser
    by Berrier, Bobby L
    Published 1986

    Government Document Book
  7. 7
    Internal performance of two nozzles utilizing gimbal concepts for thrust vectoring
    by Berrier, Bobby L
    Published 1990

    Government Document Book
  8. 8
    Effect of several geometric parameters on the static internal performance of three nonaxisymmetric nozzle concepts /
    by Berrier, Bobby L
    Published 1979

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  9. 9
    Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft /
    by Berrier, Bobby L
    Published 1980

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  10. 10
    Static performance of an axisymmetric nozzle with post-exit vanes for multiaxis thrust vectoring /
    by Berrier, Bobby L
    Published 1988

    Government Document Book
  11. 11
    Transonic aerodynamic characteristics of powered models of several Apollo launch-escape vehicle configurations /
    by Berrier, Bobby L
    Published 1968

    Book
  12. 12
    Effect of nonlifting empennage surfaces on single-engine afterbody/nozzle drag at Mach numbers from 0.5 to 2.2 /
    by Berrier, Bobby L
    Published 1977

    Government Document Book
  13. 13
    Off-design performance of two isentropic plug nozzles designed for a pressure ratio of 16.5 /
    by Berrier, Bobby L
    Published 1967

    Book
  14. 14
    Effect of plug and shroud geometry variables on plug-nozzle performance at transonic speeds /
    by Berrier, Bobby L
    Published 1969

    Book
  15. 15
    Operating characteristics of the multiple critical venturi system and secondary calibration nozzles used for weight-flow measurements in the Langley 16-foot transonic tunnel
    by Berrier, Bobby L
    Published 1985

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  16. 16
    Static internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to 60° /

    Government Document Book
  17. 17
    Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft /

    Government Document Book
  18. 18
    Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles /

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  19. 19
    Transonic aerodynamic characteristics of powered models of several Apollo launch-escape vehicle configurations /

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  20. 20
    Investigation of installation effects on single-engine convergent-divergent nozzles /
    by Burley, James R
    Published 1982
    Other Authors: “...Berrier, Bobby L...”

    Government Document Book
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