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  • Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability [microform] / George T. Carson, Jr., and Francis J. Capone.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1991.
    • 1991

  • Comparison of 3D computation and experiment for non-axisymmetric nozzles [microform] / H. Lai and E. Nelson.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • The inviscid axisymmetric stability of the supersonic flow along a circular cylinder [microform] / Peter W. Duck.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • Numerical studies of the effects of jet-induced mixing on liquid-vapor interface condensation [microform] / Chin-Shun Lin.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • The flow induced by the coalescence of two initially stationary drops [microform] / M.R. Nobari and G. Tryggvason.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Numerical simulation of shock-induced combustion past blunt bodies using shock-fitting technique [microform] : progress report for the period ended June 30, 1994 / by J.K. Ahuja, D.J. Singh, and S.N. Tiwari, principal investigator.

    • Text
    • Norfolk, Va. : Old Dominion University Research Foundation ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Marangoni convection in a gravity-free silicon float zone [microform] / by Samuel Ohring, Hans J. Lugt.

    • Text
    • Bethesda, Md. : Carderock Division, Naval Surface Warfare Center ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Supersonic jet noise reductions predicted with increased jet spreading rate [microform] / Milo D. Dahl and Philip J. Morris.

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

  • Simulations of turbulent mixing and reacting flows and their applications to turbulence modeling [microform] : semiannial progress report / Joel H. Ferziger, Brian J. Cantwell, principal investigators.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • A panel method study of vortex sheets with special emphasis on sheets of axisymmetric geometry [microform] / Ichiro Sugioka and Sheila E. Widnall.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • An outflow boundary condition for aeroacoustic computations [microform] / M. Ehtesham Hayder, Thomas Hagstrom.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, Ohio Aerospace Institute, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Enhanced mixing of an axisymmetric jet by aerodynamic excitation [microform] / Ganesh Raman.

    • Text
    • Cleveland, Ohio : Lewis Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1986]
    • 1986

  • Transition and mixing in axisymmetric jets and vortex rings [microform] / Gary A. Allen, Jr., and Brian J. Cantwell.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1986.
    • 1986

  • Characteristics of an axisymmetric sudden expansion flow [microform] : progress report, 1 Jul. 1984 - 1 Jul. 1985 / W.H. Stevenson,and H.D. Thompson.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • The design/analysis of flows through turbomachinery [microform] : a viscous/inviscid approach / D.P. Miller and D.R. Reddy.

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
    • 1991

  • A turbulence model for the NPARC code [microform] / J. Zhu and T.H. Shih.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Inlet flow test calibration for a small axial compressor rig. Part II, CFD compared with experimental results [microform] / D.P. Miller and P.S. Prahst.

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

  • Prediction of pressurant mass requirements for axisymmetric liquid hydrogen tanks [microform] / N.T. Van Dresar.

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

  • Numerical simulations of the flow in the HYPULSE expansion tube [microform] / Gregory J. Wilson, Myles A. Sussman, and Robert J. Bakos.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Computer program BL2D for solving two-dimensional and axisymmetric boundary layers / Venkit Iyer.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, VA : National Technical Information Service, distributor, 1995]
    • 1995

  • Numerical investigations in the backflow region of a vacuum plume [microform] : performance report, May 1994 - August 1995 / by Goang-Shin Liaw, principal investigator.

    • Text
    • Normal, Ala. : Alabama A&M University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Rapid numerical simulation of viscous axisymmetric flow fields [microform] / Daniel L. Tweedt and Rodrick V. Chima.

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

  • Off-design computer code for calculating the aerodynamic performance of axial-flow fans and compressors [microform] : user's manual / James F. Schmidt.

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

  • Spreading characteristics and thrust of jets from asymmetric nozzles [microform] / K.B.M.Q. Zaman.

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

  • Calculations of diffuser flows with an anisotropic K-[epsilon] model [microform] / J. Zhu and T.H. Shih.

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

  • Experimental study of vortex breakdown in a cylindrical, swirling flow [microform] / J.L. Stevens ... [et al.].

    • Text
    • [Stanford, Calif.] : Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center : Joint Institute for Aeronautics and Acoustics, Stanford University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Comparison of turbulence models for nozzle-afterbody flows with propulsive jets [microform] / William B. Compton III.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Computations of axisymmetric flows in hypersonic shock tubes [microform] / Surendra P. Sharma and Gregory J. Wilson.

    • Text
    • Washington, DC : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies [microform] / Irina G. Brykina, Carl D. Scott.

    • Text
    • Houston, Tex. : National Aeronautics and Space Administration, Lyndon B. Johnson Space Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Self-similar compressible free vortices [microform] / Karl von Ellenrieder.

    • Text
    • [Stanford, Calif.] : Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center : Joint Institute for Aeronautics and Acoustics, Stanford University ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Development and validation of a supersonic helium-air coannular jet facility [microform] / Atherton A. Carty and Andrew D. Cutler.

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

  • Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability [microform] / Mary L. Mason and James R. Burley II.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986.
    • 1986

  • The filtered Abel transform and its application in combustion diagnostics [microform] / Zeng-Guang Yuan.

    • 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/LPS55247

  • Computing axisymmetric jet screech tones using unstructured grids [microform] / Philip C.E. Jorgenson, Ching Y. Loh ; prepared for the 38th Joint Propulsion Conference and Exhibit sponsored by the AIAA, ASME, SAE, and ASEE, Indianapolis, Indiana, July 7-10, 2002.

    • 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, 2002]
    • 2002
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS56492

  • 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

  • A review of internal combustion engine combustion chamber process studies at NASA Lewis Research Center [microform] / Harold J. Schock.

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

  • Measured pressure distributions inside nonaxisymmetric nozzles with partially deployed thrust reversers / Robert S. Green, George T. Carson, Jr.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
    • 1987
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS112156

  • Measured pressure distributions inside nonaxisymmetric nozzles with partially deployed thrust reversers [microform] / Robert S. Green, George T. Carson, Jr.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
    • 1987
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS112156

  • Perormance comparison of axisymmetric and three-dimensional hydrogen film coolant injection in a 110N hydorgen-oxygen rocket [microform] / Lynn A. Arrington and Brian D. Reed.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1992?]
    • 1992

  • Modeling sound propagation through non-axisymmetric jets / Stewart J. Leib.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, March 2014.
    • 2014-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo55824

  • Calculations of diffuser flows with an anisotropic K-[epsilon] model / . Zhu and T.-H. Shih.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space AdministrationLewis Research Center, November 1995.
    • 1995-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo67332

  • Calculation of laminar heating rates on three-dimensional configurations using the axisymmetric analogue / H. Harris Hamilton II.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, September1980.
    • 1980-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo70978

  • AGCE related studies of baroclinic flows in spherical geometry / by J.M. Hyun, principal investigator.

    • Text
    • [Huntsville, Alabama] : NASA Marshall Space Flight Center, November 1983.
    • 1983-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo78302

  • An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies / Irina G. Brykina, Carl D. Scott.

    • Text
    • Houston, Texas : National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, May 1998.
    • 1998-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo83038

  • Evaluation of full Reynolds stress turbulence models in FUN3D / Julianne C. Dudek, Jan-Renee Carlson.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2017.
    • 2017-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo85654

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