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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

Analytical determination of propeller performance degradation due to ice accretion

Miller, Thomas L.
Cleveland, Ohio : Sverdrup Technology, Inc. : Lewis Research Center, [1986] 1986

Application of a Runge-Kutta scheme for high-speed inviscid internal flows

Moitra, Anutosh.
Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center Universities Space Research Association, [1986] 1986

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

Calculation of laminar heating rates on three-dimensional configurations using the axisymmetric anal

Hamilton, H. Harris, author.
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, September1980. 1980-

Enhanced viscous flow drag reduction using acoustic excitation final report

Nagel, R. T.
Hampton, Va. : NASA Langley Reasearch Center, [1988?] 1988

Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 de

Prabhu, Ramadas K.
Hampton, Va. : National Aeronautics and Science Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001] 2001

Inviscid spatial stability of a compressible mixing layer.

Jackson, Thomas L. (Thomas Luther), 1957-
Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, [1989] 1989

The inviscid stability of supersonic flow past a sharp cone

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

On computations of the integrated space shuttle flowfield using overset grids final report

Chiu, I.-T.
[Ames, Iowa] : Iowa State University, Engineering Research Institute ; [Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; Springfield, Va. : National Technical Information Service, distributor, 1990] 1990

The stability of two-dimensional wakes and shear-layers at high Mach numbers

Papageorgiou, D. T.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990] 1990

Stable boundary conditions for Cartesian grid calculations

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

WIND : computer program for calculation of three-dimensional potential compressible flow about wind

Dulikravich, George S., author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, October 1980. 1980-