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  • A high order discontinuous Galerkin method for 2D incompressible flows [microform] / Jian-Guo Liu, Chi-Wang Shu.

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

  • An inviscid computational study of an X-33 configuration at hypersonic speeds [microform] / Ramadas K. Prabhu.

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

  • Unstructured grid Euler method assessment for longitudinal and lateral/directional stability analysis of the HSR Reference H configuration at transonic speeds [microform] / Farhad Ghaffari.

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

  • Numerical flux formulas for the Euler and Navier-Stokes equations [microform] / William J. Coirier and Bram van Leer.

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

  • 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

  • Towards enhancing and delaying disturbances in free shear flows [microform] / W.O. Criminale, T.L. Jackson, D.G. Lasseigne.

    • 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 axisymmetric analog two-layer convective heating procedure with application to the evaluation of space shuttle orbiter wing leading edge and windeward surface heating [microform] / K.C. Wang.

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

  • Interface behavior of a multi-layer fluid ocnfiguration subject to acceleration in a microgravity environment [microform] : supplement I / M.J. Lyell, p.i., M. Roh.

    • Text
    • Morgantown, WV : Mechanical and Aerospace Engineering Dept., West Virginia University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • Nonlinear effects on the natural modes of oscillation of a finite length inviscid fluid column [microform] : supplement II / M.J. Lyell, p.i., L. Zhang.

    • Text
    • Morgantown, WV : Mechanical & Aerospace Engineering Dept., West Virginia University ; [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

  • Theory of finite disturbances in a centrifuglal compression system with a vaneless radial diffuser [microform] / F.K. Moore.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990

  • Inviscid spatial stability of a compressible mixing layer. Part II, The flame sheet model [microform] / T.L. Jackson, C.E. Grosch.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • Aerodynamics of engine-airframe interaction [microform] : final report / David A. Coughey.

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

  • Multigrid calculation of three-dimensional turbomachinery flows [microform] / David A. Caughey.

    • Text
    • Ithaca, New York : Fluid Dynamics and Aerodynamics Program, Sibley School of Mechanical and Aerospace Engineering, Cornell University ; [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • An approximate Riemann solver for thermal and chemical nonequilibrium flows [microform] / Ramadas K. Prabhu.

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

  • Entropy jump across an inviscid shock wave [microform] / Manuel D. Salas, Angelo Iollo.

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

  • Simple numerical method for predicting steady compressible flows [microform] : progress report for the period ended November 14, 1986 / by Ernst von Lavante, principal investigator, and N. Duane Nelson.

    • Text
    • Norfolk, Va. : Dept. of Mechanical Engineering and Mechanics, College of Engineering, Old Dominion University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1986

  • Viscous wing theory development [microform] : final report.

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

  • On similarity solutions of a boundary layer problem with an upstream moving wall [microform] / M.Y. Hussaini, W.D. Lakin, A. Nachman.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993

  • Spectral methods in fluid dynamics [microform] / M.Y. Hussaini, T.A. Zang.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • The calculation of the mass moment of inertia of a fluid in a rotating rectangular tank [microform].

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1977?]
    • 1977

  • Supercomputer implementation of finite element algorithms for high speed compressible flows [microform] : progress report for the period ended June 30, 1986 / by Earl A. Thornton, principal investigator and R. Ramakrishnan, graduate research assistant.

    • Text
    • Norfolk, Va. : Old Dominion University Research Foundation ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Large perturbation flow field analysis and simulation for supersonic inlets [microform] : final report / by M.O. Varner ... [et al.].

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1984]
    • 1984

  • Multigrid solution strategies for adaptive meshing problems [microform] / Dimitri J. Mavriplis.

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

  • GRUMFOIL, a computer code for the viscous transonic flow over airfoils [microform] / H.R. Mead and R.E. Melnik.

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

  • An improved viscid/inviscid interaction procedure for transonic flow over airfoils [microform] / R.E. Melnik ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1985.
    • 1985

  • The design/analysis of flows through turbomachinery [microform] : a viscous/inviscid approach / D.P. Miller and D.R. Reddy.

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
    • 1991

  • Parametrics on 2D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet [microform] / M. Mizukami and J.D. Saunders.

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

  • Pressure updating methods for the steady-state fluid equations [microform] / A. Fiterman, E. Turkel, V. Vatsa.

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

  • Development of a linearized unsteady Euler analysis for turbomachinery blade rows [microform] / Joseph M. Verdon, Matthew D. Montgomery, and Kenneth A. Kourson.

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

  • A numerical method for solving the three-dimensional parabolized Navier-Stokes equations [microform] / Domenic D'Ambrosio, Roberto Marsilio.

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

  • Numerical simulation of supersonic and hypersonic inlet flow fields [microform] : final report / D. Scott McRae.

    • Text
    • Raleigh, N.C. : Mars Mission Research Center, North Carolina State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Wing-section optimization for supersonic viscous flows [microform] : abstract / Cem C. Item.

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

  • Multigrid methods for aerodynamic problems in complex geometries [microform] : final report / principal investigator: David A. Caughey.

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

  • A mixed volume grid approach for the Euler and Navier-Stokes equations [microform] / William J. Coirier and Philip C.E. Jorgenson.

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

  • Methodology for simulation of unsteady flows to determine the time-dependent interference between stationary and moving boundaries [microform] : [abstract / Kamakhya Prasad Singh].

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

  • The nonlinear evolution of inviscid Gortler vortices in three-dimensional boundary layers [microform] / Nicholas Blackaby, Andrew Dando, Philip Hall.

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

  • Implicit method for the computation of unsteady flows on unstructured grids [microform] / V. Venkatakrishnan, 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, 1995]
    • 1995

  • Aeroelastic calculations using CFD for a typical business jet model [microform] / Michael D. Gibbons.

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

  • Computational study of a McDonnell Douglas single-stage-to-orbit vehicle concept for aerodynamic analysis [microform] / Ramadas K. Prabhu.

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

  • Singularities in the classical Rayleigh-Taylor flow [microform] : formation and subsequent motion / S. Tanveer.

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

  • Some approaches towards constructing optimally efficient multigrid solvers for the inviscid flow equations [microform] / David Sidilkover.

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

  • Aerodynamic design optimization on unstructured grids with a continuous adjoint formulation [microform] / W. Kyle Anderson, V. Venkatakrishnan.

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

  • Study of the velocity gradient tensor in turbulent flow [microform] / Wei-Ping Cheng and Brian Cantwell.

    • 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

  • 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

  • Aeroheating predictions for X-34 using an inviscid-boundary layer method [microform] / Christopher J. Riley and William L. Kleb, Steven J. Alter.

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

  • Solution-adaptive Cartesian cell approach for viscous and inviscid flows [microform] / William J. Coirier and Kenneth G. Powell.

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

  • Wave number selection for incompressible parallel jet flows periodic in space [microform] / Jeffrey Hilton Miles.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Evaluation of 3D inverse code using rotor 67 as test case [microform] : final report / T. Dang.

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

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