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Applications of the Lattice Boltzmann method to complex and turbulent flows

Luo, Li-Shi.
Hampton, Va. : ICASE, NASA Langley Research Center ; Springfield, Va. : For sale by the National Technical Informaton Service, [2002] 2002

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 ROT22 DATAMAP interface

Shenoy, K. R.
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1986] 1986

A dual potential formulation of the Navier-Stokes equations

Gegg, S. G., author.
[Ames, Iowa ] : Heat Transfer Laboratory, Engineering Research Institute, Iowa State University ; Moffett Field, California : NASA-Ames Research Center, [1989?] 1989

The effects of Reynolds number, motor incidence angle and surface roughness on the heat transfer dis

Blair, M. F.
East Hartford, Conn. : United Technologies Research Center ; [Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, Goerge C. Marshall Space Flight Center ; Springfield, Va. : National Technical Information Service, distributor, 1991] 1991

Extension of a three-dimensional viscous wing flow analysis

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

Extension of a three-dimensional viscous wing flow analysis user's manual : VISTA 3-D code

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

Force evaluation in the lattice Boltzmann method involving curved geometry

Hampton, Va. : ICASE, NASA Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 2002] 2002

Implementation of a transition model in a NASA code and validation using heat transfer data on a tur

Ameri, Ali A., author.
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012] 2012

An initial investigation into methods of computing transonic aerodynamic sensitivity coefficients se

Carlson, Leland A.
College Station, Tex. : Aerospace Engineering Dept., Texas A&M University ; [Washington, D.C. : National Aeronautics and Space Administration, 1991] 1991

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

Multigrid calculations of 3-D turbulent viscous flows

Yokota, Jeffrey W.
[Cleveland, Ohio] : Lewis Research Center, [1989] 1989

Numerical simulation of particle-wave interaction in boudary layers final report for NAG-1-798

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

On a class of unsteady three-dimensional Navier Stokes solutions relevant to rotating disk flows thr

Hall, Philip.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering ; [Springfield, Va. : For sale by the National Technical Information Service. 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

Three component laser Doppler measurements in an axisymmetric jet

Kuhlman, John, 1948-
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989] 1989