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  • Parallel implementation of the discontinuous Galerkin method [microform] / Abdelkader Baggag, Harold Atkins, David Keyes

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

  • 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

  • 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

  • Flutter and forced response analyses of cascades using a two-dimensional linearized Euler solver [microform] / T.S.R. Reddy and R. Srivastava, O. Mehmed.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : Available from National Technical Information Service, [1999]
    • 1999

  • Unstructured grid Euler method assessment for longitudinal and lateral/directional aerodynamic performance analysis of the HSR technology concept airplane at supersonic cruise speeds [microform] / Farhad Ghaffari.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information ; Springfield, VA : National Technical Information Service, [distributor, 1999]
    • 1999

  • Development of a grid-independent approximate Riemann solver [microform] / by Christopher Lockwood Rumsey.

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

  • Boundary conditions for unsteady compressible flows [microform] / S.I. Hariharan and D.K. Johnson.

    • 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

  • Agglomeration multigrid for viscous turbulent flows [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, 1994]
    • 1994

  • Effects of a forward-swept front rotor on the flowfield of a counterrotation propeller [microform] / M. Nallasamy and Gary G. Podboy.

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

  • Euler solutions to nonlinear acoustics of non-lifting hovering rotor blades [microform] / J.D. Baeder.

    • 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, distributor, 1991]
    • 1991

  • Temporal-adaptive Euler/Navier-Stokes algorithm for unsteady aerodynamic analysis of airfoils using unstructured dynamic meshes [microform] / William L. Kleb, John T. Batina, Marc H. Williams.

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

  • Wind tunnel pressure study and Euler code validation of a missile configuration with 77̊ swept delta wings at supersonic speeds [microform] / Patsy S. Fulton.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • An adaptively-refined, Cartesian cell-based scheme for the Euler and Navier-Stokes equations [microform] / William John Coirier.

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

  • User's guide for ENSAERO--a multidisciplinary program for fluid/structural/control interaction studies of aircraft (release 1) [microform] / Guru P. Guruswamy.

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

  • Zonal multigrid solution of compressible flow problems on unstructured and adaptive meshes [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, 1989]
    • 1989

  • A modified restricted Euler equation for turbulent flows with mean velocity gradients [microform] / Sharath S. Girimaji, Charles G. Soeziale.

    • 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 Cartesian, cell-based approach for adaptively-refined solutions of the Euler and Navier-Stokes equations [microform] / William J. Coirer and Kenneth G. Powell.

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

  • 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

  • Euler technology assessment program for preliminary aircraft design employing SPLITFLOW code with cartesian unsructured grid method [microform] / Dennis B. Finley.

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

  • An assessment of viscous effects in computational simulation of benign and burst vortex flows on generic fighter wind-tunnel models using TEAM code [microform] / Tim A. Kinard, Brenda W. Harris, and Pradeep Raj.

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

  • On bi-grid local mode analysis of solution techniques for 3-D Euler and Navier-Stokes equations [microform] / S.O. Ibraheem and A.O. Demuren.

    • 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

  • 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

  • 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

  • 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

  • Application of the space-time conservation element and solution element method to shock-tube problem [microform] / Xiao-Yen Wang and Chuen-Yen Chow and Sin-Chung Chang.

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

  • New developments in the method of space-time conservation element and solution element-applications to two-dimensional time-marching problems [microform] / Sin-Chung Chang, Xiao-Yen Wang, and Chuen-Yen Chow.

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

  • User's guide for ECAP2D [microform] : an Euler unsteady aerodynamic and aeroelastic analysis program for two dimensional oscillating cascades / T.S.R. Reddy.

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

  • Development of upwind schemes for the Euler equations [microform] / Sukumar R. Chakravarty.

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

  • Detailed near-wake flowfield surveys with comparison to an Euler method of an aspect ratio 4 rectangular wing [microform] / M.D. Klinge, S.O. Kjelgaard and J.N. Perkins.

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

  • Minimum time attitude slewing maneuvers of a rigid spacecraft [microform] / by Feiyue Li and Peter M. Bainum.

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

  • 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

  • The construction and use of divergence free vector expansions for incompressible fluid flow calculations [microform] : [final report] / Nessan Mac Giolla Mhuiris.

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

  • Implementation of a parallel unstructured Euler solver on the CM-5 [microform] / E. Morano, 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

  • Evaluation of a doubly-swept blade tip for rotorcraft noise reduction [microform] / Brian E. Wake and T. Alan Egolf.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • Contribution to the optimal shape design of two-dimensional internal flows with embedded shocks [microform] / Angelo Iollo, Manuel D. Salas.

    • 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 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

  • The method of space-time conservation element and solution element-applications to one-dimensional and two-dimensional time-marching flow problems [microform] / Sin-Chung Chang, Xiao-Yen Wang and Chuen-Yen Chow.

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

  • Investigation of convection and pressures treatment with splitting techniques [microform] / Siddharth Thakur, Wei Shyy, Meng-Sing Liou.

    • 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

  • 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

  • An LU-SSOR scheme for the Euler and Navier-Stokes equations [microform] / Seokkwan Yoon.

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

  • An multigrid LU-SSOR scheme for approximate Newton iteration applied to the Euler equations [microform] / Seokkwan Yoon and Antony Jameson.

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

  • A minimum entrophy principle in the gas dynamics equations [microform] / Eitan Tadmore.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1986]
    • 1986

  • 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

  • Effect of density gradients in confined supersonic shear layers [microform] / Oshin Peroomian and R.E. Kelly.

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

  • 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

  • An approach to the development of numerical algorithms for first order linear hyperbolic systems in multiple space dimensions [microform] : the constant coefficient case / John W. Goodrich.

    • 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

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