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  • Implicit flux-split Euler schemes for unsteady aerodynamic analysis involving unstructured dynamic meshes [microform] / John T. Batina.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990

  • Development of unstructured grid methods for steady and unsteady aerodynamic analysis [microform] / John T. Batina.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
    • 1990

  • Three-dimensional flux-split Euler schemes involving unstructured dynamic meshes [microform] / John T. Batina.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
    • 1990

  • A fast implicit upwind solution algorithm for three-dimensional unstructured dynamic meshes [microform] / John T. Batina.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
    • 1991

  • Unstructured-grid methods development, lessons learned [microform] / John T. Batina.

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

  • CFD methods development considerations for unsteady aerodynamic analysis [microform] / John T. Batina.

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

  • Implicit upwind-Euler solution algorithms for unstructured-grid applications [microform] / John T. Batina.

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

  • Progress in unstructured-grid methods development for unsteady aerodynamic applications [microform] / John T. Batina.

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

  • A gridless Euler/Navier-Stokes solution algorithm for complex two-dimensional applications [microform] / John T. Batina.

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

  • A gridless Euler/Navier-Stokes solution algorithm for complex-aircraft applications [microform] / John T. Batina.

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

  • A finite-difference approximate-factorization algorithm for solution of the unsteady transonic small-disturbance equation [microform] / John T. Batina.

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

  • Unsteady transonic flow calculations for wing-fuselage configurations [microform] / John T. Batina.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1986]
    • 1986

  • Transonic calculation of airfoil stability and response with active controls [microform] / J. T. Batina, T. Y. Yang.

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

  • Unsteady transonic flow calculations for two-dimensional canard-wing configurations with aeroelastic applications [microform] / John T. Batina.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985

  • Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads [microform] / John T. Batina.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS96402

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