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  1. 1
    First NASA/Industry High Speed Research Program Nozzle Symposium

    First NASA/Industry High Speed Research Program Nozzle Symposium

    Published 1999
    Government Document Conference Proceeding Microfilm Book
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  2. 2
    Experimental and computational investigation of a translating-throat, single-expansion-ramp nozzle

    Experimental and computational investigation of a translating-throat, single-expansion-ramp nozzle by Deere, Karen A.

    Published 1999
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    Government Document Book
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  3. 3
    Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20 /

    Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20 / by Carson, George T., Lamb, Milton

    Published 1988
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  4. 4
    Use of the PARC code to estimate the off-design transonic performance of an over/under turboramjet nozzle

    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 Microfilm Book
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  5. 5
    An approximate theoretical method for modeling the static thrust performance of non-axisymmetric two-dimensional convergent-divergent nozzles

    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 Microfilm Book
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  6. 6
    Internal performance characteristics of thrust-vectored axisymmetric ejector nozzels

    Internal performance characteristics of thrust-vectored axisymmetric ejector nozzels by Lamb, Milton

    Published 1995
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  7. 7
    SRM internal flow test and computational fluid dynamic analyses final report : contract NAS8-39095 /

    SRM internal flow test and computational fluid dynamic analyses final report : contract NAS8-39095 /

    Published 1995
    Government Document Microfilm Book
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  8. 8
    Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure

    Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure by Jankovsky, Robert S.

    Published 1996
    Government Document Microfilm Book
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  9. 9
    Initial flight test evaluation of the F-15 ACTIVE axisymmetric vectoring nozzle performance

    Initial flight test evaluation of the F-15 ACTIVE axisymmetric vectoring nozzle performance by Orme, John S.

    Published 1998
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