Research Catalog

  • Steady secondary flows generated by periodic compression and expansion of an ideal gas in a pulse tube [microform] / Jeffrey M. Lee.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999
  • Analysis and design of numerical schemes for gas dynamics 2 [microform] : artificial diffusion, discrete shock structure / Antony Jameson.

    • Text
    • [Moffett Field, Calif.] : Research Institute for Advanced Computer Science, NASA Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • Steady and unsteady three-dimensional transonic flow computations by integral equation method [microform] : final technical report / by Hong Hu, principal investigator.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • Numerical solution of the incompressible Navier-Stokes equations [microform] / Stuart E. Rogers.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990
  • Small-amplitude disturbances in turbomachine flows with swirl [microform] / David W. Wundrow.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • A perspective on unstructured grid flow problem solvers [microform] / V. Venkatakrishnan.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Multiwire thermocouples [microform] : frequency response / L.J. Forney, G.C. Fralick.

    • Text
    • [Atlanta, GA] : Georgia Institute of Technology ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • Multigrid method for a vortex breakdown simulation [microform] / Shlomo Taʹasan.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986
  • On the Lagrangian method for steady and unsteady flow [microform] / W.H. Hui and H.J. Van Roessel.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986
  • A numerical study of incompressible juncture flows [microform] / Dochan Kwak ... [et al.].

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1986]
    • 1986
  • A 3D agglomeration multigrid solver for the Reynolds-averaged Navier-Stokes equations on unstructured meshes [microform] / D.J. Mavriplis, V. Venkatakrishnan.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Efficient solutions of two-dimensional incompressible steady viscous flows [microform] / J.H. Morrison, M. Napolitano.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986
  • Application of viscous-inviscid interaction methods to transonic turbulent flows [microform] / by D. Lee, R.H. Pletcher.

    • Text
    • [Ames, Iowa] : Iowa State University. Engineering Research Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986
  • Rapid calibration of seven-hole probes [microform] / A.L. Ericksen ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • A far-field non-reflecting boundary condition for two-dimensional wake flows [microform] / Jeffrey S. Danowitz, Saul A. [i.e. S.] Abarbanel, Eli Turkel.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Direct numerical simulation of acoustic waves interacting with a shock wave in a quasi-1D convergent-divergent nozzle using an unstructured finite volume algorithm [microform] / Trong T. Bui and Reda R. Mankbadi.

    • 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
  • An accuracy assessment of Cartesian-mesh approaches for the Euler equations [microform] / William J. Coirier and Kenneth G. Powell.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995-1995
  • Static flow characteristics of a mass flow injecting valve [microform] / Duane Mattern and Dan Paxson.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Fast algorithms for visualizing fluid motion in steady flow on unstructured grids [microform] / S.K. Ueng, K. Sikorski, Kwan-Liu Ma.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Forced convection and sedimentation past a flat plate [microform] / by Nikolaos A. Pelekasis and Andreas Acrivos.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • High data density temperature measurement for quasi steady-state flows [microform] / Carolyn R. Mercer, Nasser Rashidnia, Katherine Creath.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Application of the pressure sensitive paint technique to steady and unsteady flow [microform] / Y. Shimbo, R. Mehta, B. Cantwell.

    • Text
    • [Stanford, Calif.?] : Joint Institute for Aeronautics and Acoustics ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • 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
  • An experimental investigation of steady and unsteady flow field in an axial flow turbine [microform] / M. Zaccaria 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
  • Visualizing time-varying phenomena in numerical simulations of unsteady flows [microform] / David A. Lane.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • A generalized fluid system simulation program to model flow distribution in fluid networks [microform] : draft paper ... / Alok Majumdar ... [et al.].

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998
  • Calculations of steady and transient channel flows with a time-accurate L-U factorization scheme [microform] / S.-W. Kim.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS59857
  • ULTRA-SHARP nonoscillatory convection schemes for high-speed steady multidimensional flow [microform] / B.P. Leonard and Simin Mokhtari.

    • Text
    • [Washington, D.C.] : NASA ; [Cleveland, Ohio] : Institute for Computational Mechanics in Propulsion, NASA Lewis Research Center, Case Western Reserve University ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67518
  • Unsteady three-dimensional marginal separation, including breakdown [microform] / Peter W. Duck.

    • Text
    • [Washington, D.C.] : NASA ; [Cleveland, Ohio] : Institute for Computational Mechanics in Propulsion, NASA Lewis Research Center, Case Western Reserve University ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67526
  • Shock conditions and shock wave structures in a steady flow in a dissipative fluid [microform] / Paul Germain and Jean-Pierre Guiraud.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, [1983]
    • 1983
  • Current capabilities and future directions in computational fluid dynamics [electronic resource] / Committee to Assess Current Capabilities and Future Directions in Computational Fluid Dynamics, Aeronautics and Space Engineering Board, Commission on Engineering and Technical Systems, National Research Council.

    • Text
    • Washington, D.C. : National Academy Press : Available from Aeronautics and Space Engineering Board, National Research Council, 1986.
    • 1986
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS113728
  • Current capabilities and future directions in computational fluid dynamics [microform] / Committee to Assess Current Capabilities and Future Directions in Computational Fluid Dynamics, Aeronautics and Space Engineering Board, Commission on Engineering and Technical Systems, National Research Council.

    • Text
    • Washington, D.C. : National Academy Press : Available from Aeronautics and Space Engineering Board, National Research Council, 1986.
    • 1986
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS113728
  • Performance tests for the NASA Ames Research Center 20 cm x 40 cm oscillating wind tunnel [microform] : progress report / William J. Cook and Tim A. Giddings.

    • Text
    • Ames, Iowa : Engineering Research Institute, Iowa State University, [1984]
    • 1984
  • An experimental study of airfoil-spoiler aerodynamics [microform] / Blair G. McLachlan and K. Karamcheti.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1985]
    • 1985
  • 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
  • The influence of unsteadiness on the analysis of pressure gain combustion devices / Daniel E. Paxson, Tom Kaemming.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, January 2013.
    • 2013-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo51821

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