Research Catalog

New! Try our Article Search to discover online journals, books, and more from home with your library card.

Selected filters.Clear Filters

  • 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

  • Theoretical studies of a molecular beam generator [microform] : progress report for the period ended May 15, 1994 / by John Heinbockel, principal investigator.

    • Text
    • Norfolk, Va. : Dept. of Mathematics & Statistics, College of Sciences, Old Dominion University ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Experimental investigation of nozzle/plume aerodynamics at hypersonic speeds [microform] / David W. Bogdanoff.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Experimental studies of shock-wave/wall-jet interaction in hypersonic flow [microform] / Michael S. Holden, Kathleen Rodriguez.

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

  • Computational study of generic hypersonic vehicle flow field [microform] / Johnny R. Narayan.

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

  • Enhancement of mixing in a rectangular jet by mechanical tabs [microform] / W.H. Brown and K.K. Ahuja.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, [1990]
    • 1990

  • [FDNS code to predict wall heat fluxes or wall temperatures in rocket nozzles] [microform] : final report / prepared by Gerald R. Karr.

    • Text
    • Huntsville, AL : University of Alabama in Huntsville ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993

  • 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

  • The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios [microform] / Kenneth J. Kacynski and Joe D. Hoffman.

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

  • Experimental and analytical studies of flow through a ventral and axial exhaust nozzle system for STOVL aircraft [microform] / Barbara S. Esker and James R. DeBonis.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • Shear flow control of cold and heated rectangular jets by mechanical tabs [microform] / W.H. Brown and K.K. Ahuja.

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

  • 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

  • Fluid spray simulation with two-fluid nozzles [microform] / Robert D. Ingebo.

    • Text
    • [Washington, DC] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, distributor, 1988]
    • 1988

  • Turbulence modelling of flow fields in thrust chambers [microform] : final technical report for the period June 10, 1991 through September 13, 1992 / prepared by C.P. Chen, Y.M. Kim, H.M. Shang.

    • Text
    • [Huntsville, Ala.] : Research Institute, the University of Alabama in Huntsville ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993

  • Radiative interactions in chemically reacting compressible nozzle flows using Monte Carlo simulations [microform] / by J. Liu and S.N. Tiwari (principal investigator).

    • Text
    • Norfolk, Va. : Institute for Computational and Applied Mechanics, Old Dominion University ; Hampton, Va. : NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • 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

  • A first scramjet study [microform] / George Emmanuel.

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

  • Experimental results for a hypersonic nozzle/afterbody flow field [microform] / Frank W. Spaid, Earl R. Keener, Frank C.L. Hui.

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

  • Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle [microform] / David J. Wing.

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

  • Numerical investigations of low-density nozzle flow by solving the Boltzmann equation [microform] / Zheng-Tao Deng, Goang-Shin Liaw, Lynn Chen Chou.

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

  • SSME main combustion chamber and nozzle flowfield analysis [microform] : final report / prepared by Richard C. Farmer ... [et al.].

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

  • 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

  • Validation of the NPARC code for nozzle afterbody flows at transonic speeds [microform] / James R. DeBonis and Nicholas J. Georgiadis, Crawford F. Smith.

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

  • Kinetic theory model predictions compared with low-thrust axisymmetric nozzle plume data [microform] / B.R. Riley and S.J. Fuhrman and P.F. Penko.

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

  • High speed nozzles task [microform] : final report / Awatef Hamed, principal investigator.

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

  • Shock tunnel studies of scramjet phenomena 1994. Supplements 11 and 12 [microform].

    • Text
    • [Brisbane, Australia] : University of Queensland ; [Washington, D.C. : National Aeronautics and Space Administration ; 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

  • Nozzle flow with vibrational nonequilibrium [microform] : final report for the period ended August 31, 1995 / by J.H. Heinbockel, principal investigator and J.G. Landry, graduate research assistant.

    • Text
    • Norfolk, Va. : Old Dominion University Research Foundation, Dept. of Mathematics & Statistics, College of Sciences ; [Washington, D.C. : National Aeronautics and Space Administration ; 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

  • 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

  • Nozzle flow with vibrational nonequilibrium [microform] / by John Gary Landry.

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

  • Three dimensional viscous flow field in an axial flow turbine nozzle passage [microform] / D. Ristiʹc and B. Lakshminarayana.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1997.
    • 1997

  • Three-dimensional Navier-Stokes analysis and redesign of an imbedded bellmouth nozzle in a turbine cascade inlet section [microform] / P.W. Giel ... [et al.].

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

  • Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring ability [microform] / David J. Wing, Charles T.L. Mills, and Mary L. Mason.

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

  • 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

  • Development of a telescoping vaned exhaust nozzle for the ASTOVL LiftFan application [microform] / Jack (Jagdish) S. Sokhey and Baily R. Vittal, David W. Lam.

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

  • Advanced space propulsion system flowfield modeling [microform] : final report : contract NAS8-40845 / by Sheldon D. Smith.

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

  • Effects of convoluted divergent flap contouring on the performance of a fixed-geometry nonaxisymmetric exhaust nozzle [microform] / Scott C. Asbury and Craig A. Hunter.

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

  • Numerical analysis of base flowfield for a four-engine clustered nozzle configuration [microform] / T.-S. Wang.

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

  • Design and checkout of a high speed research nozzle evaluation rig [microform] / Raymond S. Castner, John D. Wolter.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, VA : National Technical Information Service, distributor, [1997]
    • 1997

  • 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

  • Static and wind tunnel aero-performance tests of NASA AST separate flow nozzle noise reduction configurations [microform] / Kevin L. Mikkelsen and Timothy J. McDonald ; [prepared under contract NAS3-98021].

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

  • 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

  • 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

  • An incremental strategy for calculating consistent discrete CFD sensitivity derivatives [microform] / Vamshi Mohan Korivi ... [et al.].

    • Text
    • Hampton, VA : National Aeronautics and Space Administration, Langley Research Center ; [St. Louis, MO] : US Army Aviation Systems Command, [1992]
    • 1992
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60335

  • Hot gas ingestion test results of a two-poster vectored thrust concept with flow visualization in the NASA Lewis 9- x 15-foot low speed wind tunnel [microform] / Albert L. Johns, ... [et al.].

    • Text
    • [Cleveland, Ohio : Lewis Research Center, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS62061

  • Nonequilibrium in a low power arcjet nozzle [microform] / Dieter M. Zube and Roger M. Myers.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS65333

  • Analysis of internal flow in a ventral nozzle for STOVL aircraft [microform] / C. Frederic Smith and Jack G. McArdle ; prepared for the 26th Joint Propulsion Conference cosponsored by the AIAA, SAE, ASME, and ASEE, Orlando, Florida, July 16-18, 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/LPS69189

  • Operating characteristics of the multiple critical venturi system and secondary calibration nozzles used for weight-flow measurements in the Langley 16-foot transonic tunnel [microform] / Bobby L. Berrier, Laurence D. Leavitt, and Linda S. Bangert.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS96291

No results found from Digital Research Books Beta

Digital books for research from multiple sources world wide- all free to read, download, and keep. No Library Card is Required. Read more about the project.

digital-research-book
Explore Digital Research Books Beta