Research Catalog

  • A gas-kinetic scheme for multimaterial flows and its application in chemical reaction [microform] / Yongsheng Lian, Kun Xu.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999
  • A flux splitting scheme with high-resolution and robustness for discontinuities [microform] / Yasuhiro Wada, Meng-Sing Liou.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • Computed potential energy surfaces for chemical reactions [microform] : final technical report for cooperative agreement NCC2-478 for the funding period July 1, 1987 - January 31, 1994 / submitted to National Aeronautics and Space Administration ; prepared by Eloret Institute, Stephen P. Walch, principal investigator.

    • Text
    • Moffett Field, Calif. : The Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • 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
  • Flow diagnostics, chemically reacting turbulent flow modeling and turbulent mixing [microform] : a summary of project studies in combustion / principal investigator: Bahman Ghorashi.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Numerical mixing calculations of confined reacting jet flows in a cylindrical duct [microform] / Victor L. Oechsle, J.D. Holdeman.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • An application of a two-equation model of turbulence to three-dimensional chemically reacting flows [microform] / J. Lee.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • Advanced multi-phase flow CFD model development for solid rocket motor flowfield analysis [microform] : final report / by Paul Liaw and Yen-Sen Chen.

    • Text
    • Huntsville, AL : Engineering Sciences, Inc. ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • A fully implicit time accurate method for hypersonic combustion [microform] : application to shock-induced combustion instability / Shaye Yungster and Krishnan Radhakrishnan.

    • 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, 1994]
    • 1994
  • Analysis and modeling of subgrid scalar mixing using numerical data [microform] / Sharath S. Girimaji, Ye Zhou.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Comparison of PDF and moment closure methods in the modeling of turbulent reacting flows [microform] / Andrew T. Norris and Andrew T. Hsu.

    • 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
  • LES, DNS and RANS for the analysis of high-speed turbulent reacting flows [microform] : annual report submitted to NASA Langley Research Center : progress report ... for the period August 1, 1994-July 31, 1995 / by V. Adumitroaie ... [et al.].

    • Text
    • Buffalo, N.Y. : Turbulence Research Laboratory, School of Engineering and Applied Sciences, State University of New York at Buffalo ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995?]
    • 1995
  • Reliability enhancement of Navier-Stokes codes through convergence acceleration [microform] : final report / Charles L. Merkle, George S. Dulikravich.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Development of an upwind, finite-volume code with finite-rate chemistry [microform] / Gregory A. Molvik.

    • Text
    • San Jose, CA : MCAT Institute ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • LES, DNS, and RANS for the analysis of high-speed turbulent reacting flows [microform] : annual report submitted to NASA Langley Research Center : progress report ... for the period September 1, 1993-September 1, 1994 / by P. Givi ... [et al.].

    • Text
    • Buffalo, N.Y. : Turbulence Research Laboratory, School of Engineering and Applied Sciences, State University of New York at Buffalo ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • Computational study of flow establishment in hypersonic pulse facilities [microform] / S. Yungster, K. Radhakrishnan.

    • 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
  • Instrumentation development for study of Reynolds analogy in reacting flows [microform] / D.J. DeTurris.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Parallelization of the implicit RPLUS algorithm [microform] : final report, NASA grant NAG 3-1472 / by Paul D. Orkwis.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • LES, DNS, and RANS for the analysis of high-speed turbulent reacting flows [microform] : annual report submitted to NASA Langley Research Center : progress report ... under grant NAG 1-1122 for the period August 1, 1995 - July 31, 1996 / by P.J. Colucci, F.A. Jaberi, and P. Givi.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Quick-mixing studies under reacting conditions [microform] : under grant NAG3-1110 / May Y. Leong and G.S. Samuelsen.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Numerical simulation of high-speed turbulent reacting flows [microform] : annual report submitted to the NASA Langley Research Center, progress report on activities supported under grant NAG 1-1122 for the period August 1, 1996 - July 31, 1997 / by F.A. Jaberi ... [et al.].

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Numerical simulation of a low emissions gas turbine combustor using KIVA-II. Part I, Fuel nozzle/rich-burn zone analysis [microform] / S.L. Yang ... [et al.].

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Numerical simulation of a low emissions gas turbine combustor using KIVA-II. Part II, Quick-quench/lean-combustion zones analysis [microform] / S.L. Yang and R. Chen, M.C. Cline.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Application of chimera grid scheme to combustor flowfields at all speeds [microform] / Shaye Yungster, Kuo-Huey Chen.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997
  • Parallel ALLSPD-3D [microform] : speeding up combustor analysis via parallel processing / David M. Fricker.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration : U.S. Army, Research Laboratory ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997
  • Subgrid combustion modeling for the next generation national combustion code [microform] / Suresh Menon, Vaidyanathan Sankaran, and Christopher Stone.

    • 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/LPS55167
  • A multi-domain spectral method for supersonic reactive flows [microform] / Wai-Sun Don, David Gottlieb, and Jae-Hun Jung.

    • Text
    • Hampton, Va. : Institute for Computer Applications in Science and Engineering, National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 2002]
    • 2002
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60420
  • 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
  • Ensemble averaged probability density function (APDF) for compressible turbulent reacting flows / Tsan-Hsing Shih, Nan-Suey Liu.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo32097
  • Study of basic physical processes in liquid rocket engines / by S.T. Wu and C.P. Chen.

    • Text
    • Huntsville, AL : NASA/Marshall Space Flight Center, September 1992.
    • 1992-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo174437
  • Study of basic physical processes in liquid rocket engines [microform] / by S.T. Wu and C.P. Chen.

    • Text
    • Huntsville, AL : NASA/Marshall Space Flight Center, September 1992.
    • 1992-9
  • Wind-US user's guide / Dennis A. Yoder.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, March 2016.
    • 2016-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo68697
  • Parallel ALLSPD-3D : speeding up combustor analysis via parallel processing / David M. Fricker.

    • Text
    • Cleveland, Ohio : NASA Lewis Research Center and U.S. Army Research Laboratory, June 1997.
    • 1997-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo79351

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