Showing 1 - 20 results of 20 for search '', query time: 0.24s Refine Results
  1. 1
    Active chlorine and nitric oxide formation from chemical rocket plume afterburning
    by Leone, D. M
    Published 1994

    Government Document Book
  2. 2
    "2001: a space Odyssey" revisited--the feasibility of 24 hour commuter flights to the moon using NTR propulsion with LUNOX afterburners
    by Borowski, Stanley K
    Published 1998

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  3. 3
    Theoretical analysis of various thrust-augmentation cycles for turbojet engines /
    by Lundin, Bruce T
    Published 1950

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  4. 4
    Static performance of an auxiliary inlet ejector nozzle using an afterburning turbojet gas generator /
    by Burley, Richard R
    Published 1970

    Book
  5. 5
    Quiescent-air performance of a truncated turbojet plug nozzle with shroud and plug base flows from a common source /
    by Johns, Albert L
    Published 1969

    Book
  6. 6
    Performance and stall limits of an afterburner-equipped turbofan engine with and without inlet flow distortion /
    by Werner, Roger A
    Published 1970

    Book
  7. 7
    Noise evaluation of four exhaust nozzles for afterburning turbojet engine /
    by Darchuk, George V
    Published 1970

    Book
  8. 8
    Investigations of Combustion Properties of Liquid Fuels in a Constant Volume Bomb /
    by Fiskaa, G.
    Published 1985

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Book
  9. 9
    Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf /
    by Lamb, Milton
    Published 1996

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  10. 10
    High frequency-heated air turbojet
    by Miron, Juan Heliodoro Diaz
    Published 1986

    Government Document Book
  11. 11
    High-temperature test facility at the NASA Lewis Engine Components Research Laboratory /

    Government Document Book
  12. 12
    Measurement effects on the calculation of in-flight thrust for an F404 turbofan engine /

    Government Document Book
  13. 13
    Measurement effects on the calculation of in-flight thrust for an F404 turbofan engine
    by Conners, Timothy R
    Published 1989

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  14. 14
    High-temperature test facility at the NASA Lewis Engine Components Research Laboratory
    by Colantonio, Renato O
    Published 1990

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  15. 15
    Exhaust environment measurements of a turbofan engine equipped with an afterburner and 2D nozzle /
    by Brase, L. O, Brase, L. O
    Published 1990

    Government Document Book
  16. 16
    Exhaust environment measurements of a turbofan engine equipped with an afterburner and 2D nozzle
    by Brase, L. O
    Published 1990

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  17. 17
    Combined operations with and without afterburning for minimum fuel consumption in level flight /
    by Miele, Angelo
    Published 1959

    Book
  18. 18
    Experimental investigation in an altitude test facility of burning of excess combustibles in a rocket engine exhaust /
    by Bloomer, Harry E
    Published 1960

    Book
  19. 19
    Flight evaluation of a simplified gross thrust calculation technique using an F100 turbofan engine in an F-15 airplane /

    Government Document Book
  20. 20
    Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability /

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
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