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  • Factorizable schemes for the equations of fluid flow [microform] / David Sidilkover.

    • 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

  • A phase equation approach to boundary layer instability theory [microform] : Tollmien Schlichting waves / Philip Hall.

    • Text
    • Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • A new Reynolds stress algebraic equation model [microform] / Tsan-Hsing Shih and Jiang Zhu, John L. Lumley.

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

  • Control theory based airfoil design using the Euler equations [microform] / Antony Jameson and James Reuther.

    • Text
    • [Moffett Field, Calif.] : Research Institute for Advanced Computer Science, NASA Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • An asymptotic induced numerical method for the convection-diffusion-reaction equation [microform] / Jeffrey S. Scroggs, Danny C. Sorensen.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • On the breakup of viscous liquid threads [microform] / Demetrios T. Papagerogiou.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Modeling of nonequilibrium space plasma flows [microform] / Tamas Gombosi.

    • Text
    • Ann Arbor, Mich. : The University of Michigan, Dept. of Atmospheric, Oceanic, and Space Science, Space Physics Research Laboratory ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Computation of asymmetric supersonic flows around cones at large incidence [microform] : final report / principal investigator, David Degani.

    • Text
    • Technion City, Haifa, Israel : Technion Research & Development Foundation ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987?]
    • 1987

  • Application of Navier-Stokes code PAB3D with k-e turbulence model to attached and separated flows [microform] / Khaled S. Abdol-Hamid, B. Lakshmanan, John R. Carlson.

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

  • Development of direct-inverse 3-D method for applied aerodynamic design and analysis [microform] : semiannual progress report, July 1, 1986 - December 31, 1986 / Leland A. Carlson.

    • Text
    • College Station, Tex. : Texas Engineering Experiment Station, Aerospace Engineering Department, Texas A&M University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • A comparison of experimental and theoretical results for labyrinth gas seals [microform] / by Joseph Kirk Scharrer.

    • Text
    • College Station, Tex. : Texas A&M University, Turbomachinery Laboratories, Mechanical Engineering Dept. : [Washington, DC : National Aeronautics and Space Administration : Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • Semi-implicit and fully implicit shock-capturing methods for hyperbolic conservation laws with stiff source terms [microform] / H.C. Yee, Judy L. Shinn.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1986]
    • 1986

  • Third-moment closure of turbulence for predictions of separating and reattaching shear flows [microform] : final report on "A study of Reynolds-Stress Closure Model" / by R.S. Amano, principal investigator and Pankaj Goel, research assistant.

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

  • Robust integration schemes for generalized viscoplasticity with internal-state variables. Part I, Theoretical developments and applications [microform] / Atef F. Saleeb and Wei Li.

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

  • Robust integration schemes for generalized viscoplasticity with internal-state variables. Part II, Algorithmic developments and implementation [microform] / Wei Li, Atef F. Saleeb.

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

  • 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

  • Final report on adaptive computational methods for SSME internal flow analysis [microform] / by J. Tinsley Oden.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1986

  • Breakdown of the conservative potential equation [microform] / M.D. Salas and Clyde R. Gumbert.

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

  • Thermodynamic evaluation of transonic compressor rotors using the finite volume approach [microform] : status report, August 1986 on NASA grant no. NAG 3-593 / by Stephen Nicholson, John Moore.

    • Text
    • Blacksburg, Va. : Mechanical Engineering Dept., Virginia Polytechnic Institute and State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Application of the space-time conservation element and solution element method to two-dimensional advection-diffusion problems [microform] / Xiao-Yen Wang and Chuen-Yen Chow, Sin-Chung Chang.

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

  • The method of space-time conservation element and solution element [microform] : development of a new implicit solver / S.C. Chang ... [et al.].

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

  • 3-D unstructured method for flows past bodies in 6-DOF relative motion [microform] : preprint from proceedings of 6th International Symposium of Computational Fluid Dynamics, Japan Society of Computational Fluid Dynamics, September 4-8, 1995, Lake Tahoe, Nevada / K.P. Singh and Oktay Baysal.

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

  • Termination shock response to large-scale solar wind fluctuations [microform] / R.S. Steinolfson.

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

  • Comparison of several dissipation algorithms for central difference schemes [microform] / R.C. Swanson, R. Radespiel, E. Turkel.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Multi-dimensional asymptotically stable finite difference schemes for the advection-diffusion equation [microform] / Saul Abarbanel, Adi Ditkowski.

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

  • Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method [microform] / John W. Edwards.

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

  • Efficient gradient-based shape optimization methodology using inviscid/viscous CFD [microform] : summary of research report for the period of March 9, 1995 to March 8, 1997, grant# NCC-1-211 / by Oktay Baysal, principal investigator ; submitted by the Old Dominion University Research Foundation.

    • Text
    • Norfolk, Va. : Dept. of Aerospace Engineering, College of Engineering and Technology, Old Dominion University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • 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

  • Natural rolling responses of a delta wing in transonic and subsonic flows [microform] / Margaret A. Menzies and O. Kandil.

    • Text
    • Reston, Va. : American Institute of Aeronautics and Aeronautics ; [Washington, DC : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Unsteady, transonic flow around delta wings undergoing coupled and natural modes response : a multidisciplinary problem / by Margaret Anne Menzies ; a dissertation submitted to the Faculty of Old Dominion University in partial fulfillment of the requirement for the degree of Doctor of Philosophy, Aerospace Engineering, Old Dominion University.

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

  • Aerodynamic design on unstructured grids for turbulent flows [microform] / W. Kyle Anderson and Daryl L. Bonhaus.

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

  • A gas-kinetic scheme for reactive flows [microform] / Youg-Sheng Lian, Kun Xu.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998

  • Three-dimensional simulations of Marangoni-Benard convection in small containers by the least-squares finite element method [microform] / Sheng-Tao Yu ... [et al.].

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

  • Deterministic stress modeling of hot gas segregation in a turbine [microform] / Judy Busby ... [et al.].

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Study of two-dimensional compressible non-acoustic modeling of stirling machine type components [microform] / Roy C. Tew, Jr., Mounir B. Ibrahim.

    • 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/LPS30326

  • The P¹-RKDG method for two-dimensional Euler equations of gas dynamics [microform] / Bernardo Cockburn, Chi-Wang Shu.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center : ICASE, [1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67047

  • Investigation of advanced counterrotation blade configuration concepts for high speed turboprop systems. Task 1, Ducted propfan analysis [microform] : final report / Edward J. Hall, Robert A. Delaney, and James L. Bettner.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67939

  • A model for closing the inviscid form of the average-passage equation system [microform] / John J. Adamczyk, and Richard A. Mulac and Mark L. Celestina.

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
    • 1986

  • Three-dimensional unsteady Euler euqation solutions using flux vector splitting [microform] / David L. Whitfield.

    • Text
    • Mississippi State, MS : Mississippi State University, Dept. of Aerospace Engineering ; [Hampton, Va. : NASA Langley Research Center, 1983]
    • 1983

  • Numerical approach for the aerodynamic analysis of airfoils with laminar separation [microform] / prepared by David W. Halt and Dean R. Bristow.

    • Text
    • St. Louis, Mo. : McDonnel Douglas Corporation, McDonnel Aircraft Company ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985

  • Newton like [microform] : minimal residual methods applied to transonic flow calculations / Yau Shu Wong.

    • Text
    • Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, [1984]
    • 1984

  • Entropy condtion satisfying approximations for the full potential equations of transonic flow [microform] / Stanley Osher, Woodrow Whitlow, Jr., and Mohamed Hafez.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
    • 1984

  • The movement of water droplets in clouds around the nose of an atmospheric research aircraft [microform] / P. Feuillebois, M.F. Scibilia.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, [1983]
    • 1983

  • Aerodynamic effect of combustor inlet-air pressure on fuel jet atomization [microform] / Robert D. Ingebo.

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

  • An implicit finite-difference code for a two-equatuion turbulence model for three-dimensional flows [microform] / Upender K. Kaul.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1985]
    • 1985

  • An implicit, conservative, zonal-boundary scheme for Euler equation calculations [microform] / Man Mohan Rai.

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

  • The Upper-branch stability of compressible boundary layer flows / J.S.B. Gajjar and J.W. Cole.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; Cleveland, Ohio : Lewis Research Center, Institute for Computational Mechanics in Propulsion, [1989]
    • 1989
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS108153

  • The Upper-branch stability of compressible boundary layer flows [microform] / J.S.B. Gajjar and J.W. Cole.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; Cleveland, Ohio : Lewis Research Center, Institute for Computational Mechanics in Propulsion, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS108153

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