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  • Analysis of aerospike plume induced base-heating environment [microform] / T.-S. Wang.

    • Text
    • Reston, VA : American Institute of Aeronautics and Astronautics ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Development of three-dimensional DRAGON grid technology [microform] / Yao Zheng, Meng-Sing Liou and Kestutis C. Civinskas.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999

  • 3-D Navier-Stokes analysis of crossing, glancing shocks/turbulent boundary layer interactions [microform] / D.R. Reddy.

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

  • Unstructured grid methods for the simulation of 3D transient flows [microform] : final report for the period, 1 January 1992 - 31 December 1993 / principal investigator, K. Morgan, co-investigators, J. Peraire & J. Peirʹo.

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

  • A three dimensional mutigrid Reynolds-averaged Navier-Stokes solver for unstructured meshes [microform] / D.J. Mavriplis.

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

  • Finite element methods of analysis for 3d inviscid compressible flows [microform] : final report for the period 1 December 1989, 30 November 1990 / principal investigator Jaime Peraire.

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

  • An experimental study of the flowfield on a semispan rectangular wing with a simulated glaze ice accretion [microform] / Abdollah Khodadoust.

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

  • Final technical report on grant NAG3-1567 entitled Inlet distortion in engines on VSTOL aircraft [microform] / submitted to NASA Lewis Research Center ; principal investigator Choon S. Tan, co-investigator Edward M. Greitzer.

    • Text
    • Cleveland, OH : The 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

  • Performance analysis of three dimensional integral equation computations on a massively parallel computer [microform] : a thesis presented to the Graduate College, Hampton University ... / by Terry G. Logan.

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

  • A coupled Eulerian/Lagrangian method for the solution of three-dimensional vortical flows [microform] / by Helene M. Felici.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • A stable penalty method for the compressible Navier-Stokes equations. I., Open boundary conditions [microform] / J.S. Hesthaven, D. Gottlieb.

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

  • An aerodynamic analysis of a mixed flow turbine [microform] / Chan M. Kim and Kestutis C. Civinskas.

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

  • Surface documentation of a 3-D supersonic, shock-wave-boundary layer interaction [microform] / Jeffrey K. Wideman ... [et al.].

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

  • Flowfield of a lifting hovering rotor--a Navier-Stokes simulation [microform] / G.R. Srinivasan ... [et al.].

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center : US Army Aviation Systems Command, Aviation Research and Technology Activity ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990

  • A laser Doppler velocimeter approach for near-wall three-dimensional turbulence measurements [microform] / D.A. Johnson and J.D. Brown.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • A computational and experimental investigation of a three-dimensional hypersonic scramjet inlet flow field [microform] / by Scott Douglas Holland.

    • Text
    • Raleligh, NC : North Carolina State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • Numerical study of supersonic combustors by multi-block grids with mismatched interfaces [microform] / Young J. Moon.

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

  • A diagonally inverted LU implicit multigrid scheme for the 3-D Navier-Stokes equations and a two equation model of turbulence [microform] / Jeffrey W. Yokota.

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

  • Three dimensional viscous analysis of a hypersonic inlet [microform] / D.R. Reddy ... [et al.].

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1989?]
    • 1989

  • A prediction of 3-D viscous flow and performance of the NASA low-speed centrifugal compressor [microform] / John Moore, Joan G. 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, 1989]
    • 1989

  • Three dimensional compressible turbulent flow computations for a diffusing S-duct with/without vortex generators [microform] / by Soo-Yong Cho and Isaac Greber.

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

  • A three-dimensional structured/unstructured hybrid Navier-Stokes method for turbine blade rows [microform] / F.-L. Tsung ... [et al.].

    • 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

  • Numerical design of advanced multi-element airfoils [microform] : final report / Donovan L. Mathias, Russell M. Cummings.

    • Text
    • San Luis Obispo, CA : California Polytechnic State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • An assessment of the adaptive unstructured tetrahedral grid, Euler flow solver code FELISA [microform] / M. Jahed Djomehri, Larry L. Erickson.

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

  • Unsteady three-dimensional flow separation [microform] / W.H. Hui.

    • Text
    • Waterloo, Ont. : University of Waterloo Research Institute ; Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • Mach 10 computational study of a three-dimensional scramjet inlet flow field [microform] / Scott D. Holland.

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

  • A Note on singularities of the 3-D Euler equation [microform] : / S. Tanveer.

    • 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 three-dimensional dual potential procedure with applications to wind tunnel inlets and interacting boundary layers [microform] : final report / K.V. Rao ... [et al.].

    • Text
    • [Ames, Iowa?] : Heat Transfer Laboratory, Dept. of Mechanical Engineering, Computational Fluid Dynamics Center, Engineering Research Institute, Iowa State University ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • 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

  • AGARD fluid dynamics panel symposium on applications of computational fluid dynamics in aeronautics [microform] / W.J. McCroskey.

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

  • A numerical study of three-dimensional vortex breakdown [microform] / Robert E. Spall and Robert L. Ash.

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

  • Numerical investigations in three-dimensional internal flows [microform] : semi-annual status report, 1 April through 30 September 1988 / by William C. Rose.

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

  • Convergence acceleration of the Proteus computer code with multigrid methods [microform] : final report for the period ended January 15, 1995 / by A.O. Demuren, principal investigator and S.O. Ibrahim

    • Text
    • Norfolk, Va. : Old Dominion University Research Foundation ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • A computer code for three-dimensional incompressible flows using nonorthogonal body-fitted coordinate systems [microform] : final report / by Y.S. Chen.

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

  • Transverse vorticity measurements using an array of four hot-wire probes [microform] / John F. Foss, Casey L. Klewicki, and Peter J. Disimile.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • TranAir, a full-potential, solution-adaptive, rectangular grid code for predicting subsonic, transonic, and supersonic flows about arbitrary configurations [microform] : user's manual / F.T. Johnson ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1992.
    • 1992

  • Study by double exposure holography of the three-dimensional character of the flow around an airfoil profile in a wind tunnel [microform] / G. Heid and M. Stanislas.

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

  • A general theory of two-and three-dimensional rotational flow in subsonic and transonic turbomachines [microform] / Chung-Hua Wu.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1993.
    • 1993

  • Turbomachinery design and tonal acoustics computations [microform] / Akil A. Rangwalla.

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

  • Implicit multigrid algorithms for the three-dimensional flux split Euler equations [microform] / by William Kyle Anderson.

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

  • Nonlinear potential analysis techniques for supersonic aerodynamic design [microform] / V. Shankar and K.Y. Szema.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • Computation of multi-dimensional viscous supersonic jet flow [microform] / Y.N. Kim, R.C. Buggeln, and H. McDonald ; prepared for Lewis Research Center under contract NAS3-22759.

    • 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

  • Duct flow nonuniformities [microform] : effects of struts in SSME HGM II⁺ : final report / prepared for National Aeronautics and Space Administration, Marshall Space Flight Center, by Roger Burke.

    • Text
    • Huntsville, AL : Lockheed Missiles & Space Co., Huntsville Engineering Center ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • Calculation of water drop trajectories to and about arbitrary three-dimensional bodies lifting and nonlifting bodies in potential airflow [microform] / Hillyer G. Norment.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : National Technical Information Service, distributor], 1985.
    • 1985

  • Global flowfield about the V-22 tiltrotor aircraft [microform] : progress report for NASA cooperative agreement NCC2-747 / submitted to NASA Ames Research Center, Applied Computational Fluid Dynamics [i.e. Aerodynamics] Branch ; by Overset Methods, Inc. ; principal investigator, Dr. Robert L. Meakin.

    • Text
    • [Moffett Field, Calif.] : The Branch ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Leading edge film cooling effects on turbine blade heat transfer [microform] / Vijay K. Garg and Raymond E. Gaugler.

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

  • The decay of longitudinal vortices shed from airfoil vortex generators [microform] / Bruce J. Wendt, Bruce A. Reichert, Jeffry D. Foster.

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

  • Numerical simulation of stability and stabiity control of high speed compressible rotating couette flow [microform] : final report for NASA grant NAG-1-1103 / principal investigator, Sedat Biringen, research associate, Ferhat F. Hatay.

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

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