Showing 1 - 20 results of 24 for search '', query time: 0.21s Refine Results
  1. 1
    Initial flight test evaluation of the F-15 ACTIVE axisymmetric vectoring nozzle performance
    by Orme, John S
    Published 1998

    Government Document Book
  2. 2
    SRM internal flow test and computational fluid dynamic analyses final report : contract NAS8-39095 /
    Published 1995

    Government Document Book
  3. 3
    An approximate theoretical method for modeling the static thrust performance of non-axisymmetric two-dimensional convergent-divergent nozzles
    by Hunter, Craig A
    Published 1995

    Government Document Book
  4. 4
    Internal performance characteristics of thrust-vectored axisymmetric ejector nozzels
    by Lamb, Milton
    Published 1995

    Government Document Book
  5. 5
    Use of the PARC code to estimate the off-design transonic performance of an over/under turboramjet nozzle
    by Lam, David W
    Published 1995

    Government Document Book
  6. 6
    Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20 /
    by Carson, George T
    Published 1988

    Government Document Book
  7. 7
    Performance of a 10 deg conical plug nozzle with a stowed thrust reverser at Mach numbers from 0 to 2.0 /
    by Steffen, Fred W
    Published 1970

    Book
  8. 8
    Coolant flow effects on the performance of a conical plug nozzle at Mach numbers from 0 to 2.0 /
    by Jeracki, Robert J
    Published 1970

    Book
  9. 9
    Static performance of an auxiliary inlet ejector nozzle using an afterburning turbojet gas generator /
    by Burley, Richard R
    Published 1970

    Book
  10. 10
    Performance of convergent and plug nozzles at Mach numbers from 0 to 1.97 /
    by Harrington, Douglas E
    Published 1970

    Book
  11. 11
    Performance of an aerodynamically positioned auxiliary inlet ejector nozzle at Mach numbers from 0 to 2.0 /
    by Bresnahan, Donald L
    Published 1970

    Book
  12. 12
    Effect of nozzle lateral spacing on afterbody drag and performance of twin-jet afterbody models with convergent nozzles at Mach numbers up to 2.2 /
    by Maiden, Donald L
    Published 1970

    Book
  13. 13
    Experimental investigation of a 10 deg conical turbojet plug nozzle with translating primary and secondary shrouds at Mach numbers from 0 to 2.0 /
    by Bresnahan, Donald L
    Published 1969

    Book
  14. 14
    Decomposing solid micropropulsion nozzle performance issues
    by Reed, Brian D
    Published 2003

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  15. 15
    First NASA/Industry High Speed Research Program Nozzle Symposium
    Published 1999

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Conference Proceeding Book
  16. 16
    Analysis and testing of two-dimensional slot nozzle ejectors with variable area mixing sections /
    by Gilbert, Gerald B
    Published 1973

    Book
  17. 17
    Experimental and analytical study of close-coupled ventral nozzles for ASTOVL aircraft /
    by McArdle, Jack G, McArdle, Jack G
    Published 1990

    Government Document Book
  18. 18
    Decomposing solid micropropulsion nozzle performance issues
    by Reed, Brian D
    Published 2003

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  19. 19
    Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20 /

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  20. 20
    Decomposing solid micropropulsion nozzle performance issues /
    by Reed, Brian D, Reed, Brian D
    Published 2003

    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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