Research Catalog

  • First NASA/Industry High Speed Research Program Nozzle Symposium [microform] / proceedings of a conference held at and sponsored by NASA Glenn Research Center, Cleveland, Ohio, November 17-19, 1992.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : National Technical Information Service [distributor, 1999]
    • 1999
  • An approximate theoretical method for modeling the static thrust performance of non-axisymmetric two-dimensional convergent-divergent nozzles [microform] / Craig A. Hunter.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Internal performance characteristics of thrust-vectored axisymmetric ejector nozzels [microform] / Milton Lamb.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Use of the PARC code to estimate the off-design transonic performance of an over/under turboramjet nozzle [microform] / David W. Lam.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • SRM internal flow test and computational fluid dynamic analyses [microform] : final report : contract NAS8-39095 / prepared by ERC, Incorporated.

    • Text
    • Huntsville, AL : ERC, Inc. ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995- ]
    • 1995-present
  • Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure [microform] / Robert S. Jankovsky and John M. Kazaroff, Albert J. Pavli.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Initial flight test evaluation of the F-15 ACTIVE axisymmetric vectoring nozzle performance [microform] / John S. Orme, Ross Hathaway, Michael D. Ferguson.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998
  • Experimental and computational investigation of a translating-throat, single-expansion-ramp nozzle [microform] / Karen A. Deere and Scott C. Asbury.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999
  • Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20 [microform] / George T. Carson, Jr., and Milton Lamb.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1988.
    • 1988
  • Decomposing solid micropropulsion nozzle performance issues [microform] / Brian Reed.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from the NASA Center for Aerospace Information ; Springfield, VA : National Technical Information Service [distributor, 2003]
    • 2003
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS55253

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