Research Catalog

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  • Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept [microform] / David J. Wing.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Comparison of UNL laser imaging and sizing system and a phase Doppler system for analyzing sprays from a NASA nozzle [microform] / Dennis R. Alexander.

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

  • Two-dimensional converging-diverging rippled nozzles at transonic speeds [microform] / John R. Carlson and Scott C. Asbury.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Radiant energy measurements from a scaled jet engine axisymmetric exhaust nozzle for a baseline code validation case [microform] / Joseph F. Baumeister.

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

  • Ultra-high bypass ratio jet noise [microform] / John K.C. Low.

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

  • Investigation of ramp injectors for supersonic mixing enhancement [microform] / Y. Haimovitch, E. Gartenberg, and A.S. Roberts.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, VA : National Technical Information Service, distributor, 1994]
    • 1994

  • Aeroacoustics of supersonic jet flows from contoured and solid-porous conical plug-nozzles [microform] / Darshan S. Dosanjh and Indu S. Das.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • High performance solid rocket motor (SRM) submerged nozzle-combustion cavity flowfield assessment [microform] : final report / prepared by J.A. Freeman ... [et al.].

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • Semi annual progress report for the period June 30, 1988 - December 31, 1988 on the effects of magnetic nozzle configurations on plasma thrusters [microform] / principal investigator, Thomas M. York.

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

  • Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows [microform] / by Scott T. Imlay.

    • 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

  • 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

  • A detailed description of the uncertainty analysis for high area ratio rocket nozzle tests at the NASA Lewis Research Center [microform] / Kenneth J. Davidian, Ronald H. Dieck and Isaac Chuang ; prepared for the 24th JANNAF Combustion Meeting, Monterey, California, October 5-9, 1987.

    • Text
    • [Washington, D.C.?] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • Heat transfer predictions for two turbine nozzle geometries at high Reynolds and Mach numbers [microform] / R.J. Boyle and R. Jackson.

    • Text
    • [Washington, D.C.] : 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

  • 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

  • Aeroacoustic characteristics of a rectangular multi-element supersonic jet mixer-ejector nozzle [microform] / Ganesh Raman, Ray Taghavi.

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

  • The effects of magnetic nozzle configurations on plasma thrusters [microform] : final report, grant/contract no.: NAG3-843 / prepared by P.J. Turchi.

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

  • 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

  • Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct [microform] / David J. Wing.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998

  • CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system [microform] : final report : under contract NAG3-1500 / Ing Chuang, Louis G. Hunter.

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

  • Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes [microform] / Robert J. Foley, Odis C. Pendergraft, Jr.

    • 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

  • 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

  • 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

  • Space shuttle ice suppression system validation [microform] : volume III / J.L.F. Porteiro, D.J. Norton, and T.C. Pollock ; prepared by Texas Engineering Experiment Station, Texas A&M University.

    • Text
    • College Station, Tex. : Texas Engineering Experiment Station, Texas A&M University, [1983]
    • 1983

  • Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap [microform] / Richard J. Re and Laurence D. Leavitt.

    • 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

  • 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

  • Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility [microform] / Kin C. Wong.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Hanover, Md. : Available from the NASA Center for Aerospace Information, 2003]
    • 2003
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS55251

  • 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

  • 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

  • An experimental comparison of nonswirling and swirling flow in a circular-to-rectangular transition duct [microform] / B. A. Reichert and W. R. Hingst, and T. H. Okiishi.

    • Text
    • [Cleveland, Ohio : Lewis Research Center, 1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS62060

  • Experimental evaluation of a translating nozzle sidewall radial turbine [microform] / Richard J. Roelke and Casimir Rogo.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1987]
    • 1987
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS92422

  • Flow visualization and interpretation of visualization data for deflected thrust V/STOL nozzles [microform] / H.C. Kao, P. L. Burstadt, and A. L. Johns.

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

  • Preliminary analysis of tone-excited two-stream jet velocity decay [microform] / U. H. von Glahn.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, [1985]
    • 1985

  • 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

  • Exhaust nozzle plume effects on sonic boom test results for isolated nozzles / Raymond S. Castner ; prepared for the 28th Applied Aerodynamics Conference sponsored by the American Institute of Aeronautics and Astronautics, Chicago, Illinois, June 28-July 1, 20.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo27499

  • Proposed flight research of a dual-bell rocket nozzle using the NASA F-15 airplane / Daniel S. Jones and Trong T. Bui, Joseph H. Ruf.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, September 2013.
    • 2013-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo50963

  • Noise measurements of high aspect ratio distributed exhaust systems / James E. Bridges.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 2015.
    • 2015-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65870

  • Modeling and prediction of the noise from non-axisymmetric jets / Stewart J. Leib.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo53475

  • Assessment at full scale of nozzle/wing geometry effects on OTW aero-acoustic characteristics / D. Groesbeck and U. von Glahn.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, [January 1979]
    • 1979-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo172466

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