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  • Acoustic and aerothermal performance test of the axisymmetric coannular ejector nozzle [microform] / William Herkes.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information ; Springfield, VA : National Technical Information Service [distributor, 2000-
    • 2000

  • Noise measurements from an ejector suppressor nozzle in the NASA Lewis 9- by 15-foot low speed wind tunnel [microform] / Eugene A. Krejsa ... [et al.].

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • A control-volume method for analysis of unsteady thrust augmenting ejector flows [microform] / Colin K. Drummond.

    • Text
    • Cleveland, Ohio : Lewis Research Center, National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1988]
    • 1988

  • Experiments on high speed ejectors [microform] / J.J. Wu.

    • Text
    • [Moffett Field, Calif.] : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • 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

  • Experimental investigation of wing installation effects on a two-dimensional mixer/ejector nozzle for supersonic transport aircraft [microform] / David J. Anderson, Heather H. Lambert, and Masashi Mizukami.

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight [microform] / Scott R. Thomas, H. Douglas Perkins, and Charles J. Trefny.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Lobed mixer optimization for advanced ejector geometries [microform] : annual report and proposal for continuation of NASA contract NCC3-414 / principal investigator: Ian A. Waitz.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Combined numerical/analytical perturbation solutions of the Navier-Stokes equations for aerodynamic ejector/mixer nozzle flows [microform] : prepared under grant NGT-51244 / Lawrence Justin De Chant.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Analysis of a rocket based combined cycle engine during rocket only operation [microform] / T.D. Smith ... [et al.].

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Parametric studies of the ejector process within a turbine-based combined-cycle propulsion system [microform] / Nicholas J. Georgiadis, James F. Walker, and Charles J. Trefny.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999

  • A comparison of three Navier-Stokes solvers for exhaust nozzle flowfields [microform] / Nicholas J. Georgiadis, Dennis A. Yoder, and James R. DeBonis.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999

  • Effect of delta tabs on free jets from complex nozzles [microform] / K.B.M.Q Zaman.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS26802

  • Unsteady ejector performance [microform] : an experimental investigation using a pulsejet driver / Daniel E. Paxson, Jack Wilson and Kevin T. Dougherty.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information, [2002]
    • 2002
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS30958

  • Thrust augmentation measurements using a pulse detonation engine ejector [microform] / Robert J. Santoro and Sibtosh Pal.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS55218

  • Supersonic STOVL aircraft from a propulsion point of view [microform] / R. Luidens, ... [et al.].

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, 1984]
    • 1984
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS99449

  • Experimental investigation of an ejector-powered free-jet facility [microform] / Mary Jo Long.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, 1992]
    • 1992

  • Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight / Scott R. Thomas, H. Douglas Perkins, and Charles J. Trefny.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, March 1997.
    • 1997-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo72111

  • Multiple-cycle simulation of a pulse detonation engine ejector / S. Yungster, H.D. Perkins.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, October 2002.
    • 2002-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS53266

  • Effect of delta tabs on free jets from complex nozzles / K.B.M.Q. Zaman.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, March 2001.
    • 2001-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS26802

  • A multidisciplinary approach to mixer-ejector analysis and design / Eric S. Hendricks and Jonathan A. Seidel.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo33020

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