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  • Soobshcheni︠i︡a po prikladnoĭ matematike.

    • Moskva, Vychislitelʹnyĭ ︠t︡sentr AN SSSR, 1969-
    • 1969-present
    • 1 Item
    FormatCall NumberItem Location
    *QHA 75-328Offsite

  • Analysis of ejectors used as supersonic propelling nozzles for jet engines.

    • Text
    • Stockholm, 1968.
    • 1968
    • 1 Item
    FormatCall NumberItem Location
    Text VDYR+ (Ahren, B. Analysis of ejectors used as supersonic propelling nozzles)Offsite

  • Experimental investigation of a single flush-mounted hypermixing nozzle [microform] / David O. Davis, Warren R. Hingst and A. Robert Porro.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1991-1990

  • Progress toward synergistic hypermixing nozzles [microform] / D.O. Davis and W.R. Hingst.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, [1991]
    • 1991

  • The flip-flop nozzle extended to supersonic flows [microform] / Ganesh Raman, Michael Hailye, and Edward J. Rice.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
    • 1992

  • Computation of supersonic jet mixing noise for an axisymmetric CD nozzle using k-(epsilon) turbulence model [microform] / Abbas Khavaran and Eugene A. Krejsa and Chan M. Kim.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration, 1991]
    • 1991

  • Internal reversing flow in a tailpipe offtake configuration for SSTOVL aircraft [microform] / Jack G. McArdle and Barbara S. Esker and James A. Rhodes.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
    • 1992

  • Computation of supersonic jet noise under imperfectly expanded conditions [microform] / Chan M. Kim and Eugene A. Krejsa and Abbas Khavaran.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1993]
    • 1993

  • Generation of monodisperse droplets by spontaneous condensation of flow in nozzles [microform] : final technical report / by Der-Shaium Lai and J.R. Kadambi.

    • Text
    • Cleveland, Ohio : Dept. of Mechanical and Aeropsace [i.e. Aerospace] Engineering, Case Western University ; [Washington, D.C. : National Aeronautics and Space Administration, 1993]
    • 1993

  • Method of characteristics design of a supersonic wind tunnel nozzle with square cross-section [microform] : status report for NASA Langley grant NAG-1-113, supplement 3 / principal investigator: Steven P. Schneider.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993

  • Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle [microform] / Dr. Stephen D. Wolf.

    • Text
    • San Jose, CA : MCAT Institute ; [Washington, D.C. : National Aeronautics and Space Administration : National Technical Information Service, distributor, 1991]
    • 1991

  • Shock-free supersonic elliptic nozzles and method of forming same [microform] / inventor, John M. Seiner, inventor, Roy S. Baty.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration, 1993]
    • 1993

  • Resonant interaction of a linear array of supersonic rectangular jets [microform] : an experimental study / Ganesh Raman and Ray Taghavi.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Development of quiet-flow supersonic wind tunnels for laminar-turbulent transition research [microform] : final report / Steven P. Schneider.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle [microform] : final report / Stephen W.D. Wolf.

    • Text
    • San Jose, CA : MCAT Institute ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Three-dimensional aerodynamic shape optimization using discrete sensitivity analysis [microform] : abstract / Gregory W. Burgreen.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995?]
    • 1995

  • Final summary report under NASA cooperative agreement no. NCC10-0010 entitled "Supersonic Gas-Liquid Cleaning System" research project [microform] / principal investigator, Frank Kinney.

    • Text
    • Titusville, Fla. : Technological Research and Development Authority, State of Florida ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Screech tones of supersonic jets from bevelled rectangular nozzles [microform] / Christopher K.W. Tam and Hao Shen, Ganesh Raman.

    • Text
    • Reston, VA : American Institute of Aeronautics and Astronautics ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Computational noise study of a supersonic short conical plug-nozzle jet [microform] / Indu S. Das, Abbas Khavaran, and A.P. Das.

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

  • Near field pressure fluctuations in the exit plane of a choked axisymmetric nozzle [microform] / Michael K. Ponton, John M. Seiner, and Martha C. Brown.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • An evaluation of parameters influencing jet mixing using the WIND Navier-Stokes Code [microform] / Mary Ann Dembowski and Nicholas J. Georgiadis.

    • 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/LPS36330

  • Optical techniques for determination of normal shock position in supersonic flows for aerospace applications [microform] / Grigory Adamovsky and John G. Eustace ; prepared for the Conference on Optical Testing and Metrology III sponsored by the Society of Photo-Optical Instrumentation Engineers, San Diego, California, July 8-13, 1990.

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1990?]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS58836

  • Effects of nozzle exit geometry and pressure ratio on plume shape for nozzles exhausting into quiescent air [microform] / W.I. Scallion.

    • Text
    • Hamtpon, Va. : National Aeronautics and Space Administration, Langley Research Center : [Springfield, Va. : For sale by the National Technical Information Service, 1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60070

  • Aeroacoustic data for high Reynolds number supersonic axisymmetric jets [microform] / John M. Seiner, Michael K. Ponton.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
    • 1985

  • An automated DAKOTA and VULCAN-CFD framework with application to supersonic facility nozzle flowpath optimization / Erik L. Axdahl.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 2015.
    • 2015-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo62868

  • An evaluation of parameters influencing jet mixing using the WIND Navier-Stokes Code / Mary Ann Dembowski and Nicholas J. Georgiadis.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, August 2002.
    • 2002-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS36330

  • The design, development and testing of two-dimensional sharp-cornered supersonic nozzles / by Gilbert M. Edelman.

    • Text
    • 1948.
    • 1948
    • 1 Item
    FormatCall NumberItem Location
    Text F 4270Off-site

  • Analysis of ejectors used as supersonic propelling nozzles for jet engines.

    • Text
    • Stockholm, 1968.
    • 1968
    • 1 Item
    FormatCall NumberItem Location
    Text 92729.115qOff-site

  • Raschet ravnovesnykh techeniĭ gaza v sverkhzvukovykh soplakh / O.N. Kat︠s︡kova.

    • Text
    • Moskva : Vychislitelʹnyĭ t︠s︡entr AN SSSR, 1964.
    • 1964
    • 1 Item
    FormatCall NumberItem Location
    Text 92517.513Off-site

  • Charts for equilibrium and frozen nozzle flows of carbon dioxide, by George G. Mateer and Victor L. Peterson.

    • Text
    • Washington, Scientific and Technical Information Division, National Aeronautics and Space Administration; [for Sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.] 1965.
    • 1965
    • 1 Item
    FormatCall NumberItem Location
    Text 8384.622Off-site

  • A summary of the techniques of variable Mach number supersonic wind tunnel nozzle design, by J.T. Kenney and L.M. Webb.

    • Text
    • [Paris] North Atlantic Treaty Organization, Advisory Group for Aeronautical Research and Development, 1954.
    • 1954
    • 1 Item
    FormatCall NumberItem Location
    Text AGARDOGRAPH-3Off-site

  • A summary of the techniques of variable Mach number supersonic wind tunnel nozzle design, by J.T. Kenney and L.M. Webb.

    • Text
    • [Paris] North Atlantic Treaty Organization, Advisory Group for Aeronautical Research and Development, 1954.
    • 1954
    • 1 Item
    FormatCall NumberItem Location
    Text AGARDOGRAPH-3Off-site

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