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Accuracy of schemes for the Euler equations with nonuniform meshes

Turkel, E.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center : Institute for Computer Applications in Science and Engineering, [1985] 1985

Adaptive grid embedding for the two-dimensional flux-split Euler equations

Warren, Gary Patrick.
Mississippi State, Miss. : Mississippi State University, Dept. of Aerospace Engineering, [1990] 1990

Analysis and mitigation of numerical dissipation in inviscid and viscid computation of vortex-domina

Kandil, Osama A.
Norfolk, Va. : Dept. of Mechanical Engineering and Mechanics, College of Engineering and Technology, Old Dominion University ; [Hampton, Va. : National Aeronautics and Space Administration, 1990] 1990

An approximate method for calculating three-dimensional inviscid hypersonic flow fields

Riley, Christopher J. (Christopher Joseph), 1964-
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1990. 1990

Development of an aeroelastic code based on an Euler/Navier-Stokes aerodynamic solver

Bakhle, Milind A., author.
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, November 1996. 1996-

Error estimates for cell-vertex solutions of the compressible Euler equations

Roe, P. L., author.
Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, [1987] 1987

Euler and Navier-Stokes computations for two-dimensional geometries using unstructured meshes

Mavriplis, Dimitri.
Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990] 1990

Investigation of advanced counterrotation blade configuration concepts for high speed turboprop syst

Hall, Edward J.
[Washington, D.C.] : National Aeronautics and Space Administration, [1990] 1990

Marching iterative methods for the parabolized and thin layer Navier-Stokes equations

Israeli, Moshe.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center : Institute for Computer Applications in Science and Engineering, [1985] 1985

Shock wave interaction with an abrupt area change

Salas, Manuel D.
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1991. 1991

Some aspects of essentially nonoscillatory (ENO) formulations for the Euler equations

Chakravarthy, Sukumar R.
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1990. 1990

Stable boundary conditions and difference schemes for Navier-Stokes equations

Dutt, Pravir.
Hampton, Va. : Institute for Computer Applications in Science and Engineering, National Aeronautics and Space Administration, Langley Research Center, [1985] 1985

Stable boundary conditions for Cartesian grid calculations

Berger, Martin J., 1922-
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990] 1990

Application of Lagrangian blending functions for grid generation around airplane geometries

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