Showing 1 - 15 results of 15 for search 'Castner, Raymond S', query time: 0.16s Refine Results
  1. 1
    Exhaust nozzle plume effects on sonic boom test results for isolated nozzles /

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Conference Proceeding Book
  2. 2
    Exhaust plume effects on sonic boom for a delta wing and a swept wing-body model /
    by Castner, Raymond, Castner, Raymond
    Published 2012

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    Government Document Conference Proceeding Book
  3. 3
    Slot nozzle effects for reduced sonic boom on a generic supersonic wing section /

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    Government Document Conference Proceeding Book
  4. 4
    Background pressure profiles for sonic boom vehicle testing in the NASA Glenn 8- by 6-foot supersonic wind tunnel /

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    Government Document Book
  5. 5
    Exhaust nozzle plume effects on sonic boom test results for vectored nozzles /

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Conference Proceeding Book
  6. 6
    Wind tunnel model design for the study of plume effects on sonic boom for isolated exhaust nozzles /

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Conference Proceeding Book
  7. 7
    The nozzle acoustic test rig an acoustic and aerodynamic free-jet facility /
    by Castner, Raymond S
    Published 1994

    Government Document Book
  8. 8
    Design and checkout of a high speed research nozzle evaluation rig
    by Castner, Raymond S
    Published 1997

    Government Document Book
  9. 9
    Design and checkout of a high speed research nozzle evaluation rig /
    by Castner, Raymond S
    Published 1997

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  10. 10
    Exhaust nozzle plume and shock wave interaction /

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  11. 11
    Supersonic inlet test for a quiet supersonic transport technology demonstrator in the NASA Glenn 8-by 6-foot supersonic wind tunnel /

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  12. 12
    Supersonic inlet test for a quiet supersonic transport technology demonstrator in the NASA Glenn 8-by 6-foot supersonic wind tunnel

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Electronic Book
  13. 13
    Numerical simulations of a Quiet SuperSonic Technology (QueSST) aircraft preliminary design /

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  14. 14
    Numerical simulations of a Quiet SuperSonic Technology (QueSST) aircraft preliminary design

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Electronic Book
  15. 15
    A study of highly underexpanded supersonic jets in subsonic crossflow /

    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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