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A generalized wall function [microform] / Tsan-Hsing Shih ... [et al.].
Microform
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
1999
0 resources
Textbook multigrid efficiency for the incompressible Navier-Stokes equations [microform] : high Reynolds number wakes and boundary layers / James L. Thomas, Boris Diskin, Achi Brandt.
Microform
Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
1999
0 resources
An experimental study of a separated/reattached flow behind a backward-facing step. Re[subscript h] = 37,000 [microform] / Srba Jovic.
Microform
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Three-dimensional Navier-Stokes simulations with two-equation turbulence models of intersecting shock-waves/turbulent boundary layer at Mach 8.3 [microform] / J.E. Bardina, T.J. Coakley.
Microform
Washington, D.C. : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Growth characteristics downstream of a shallow bump [microform] : computation and experiment / Ronald D. Joslin, Chester E. Grosch.
Microform
Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate) [microform] : final report of TsAGI under cooperative agreement # NCCW-72.
Microform
Zhukovsky, Russia : Central Aero-Hydrodynamics Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Numerical study of boundary-layer control in aerodynamics [microform] : final technical report for grant NCC 2-845, NASA-Ames Research Center; grant period: 1 January 1994 to 31 December 1995, no-cost extension to 31 December 1996 / submitted by Tom I.-P. Shih.
Microform
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
A near-wall Reynolds-stress closure without wall normals [microform] : under grant NAG1-1772 / S.P. Yuan and R.M.C. So.
Microform
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate) [microform] : under cooperative agreement NCC1-241 / M.N. Kogan and M.V. Ustinov.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Supersonic laminar flow control research [microform] : NASA grant no. NAG 2-881, final report, January 1994 - June 1996 / principal investigator, Ching F. Lo; other investigators [i.e. investigator], Clark G. Wiberg.
Microform
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Effect of flow misalignment and multi-hole interaction on boundary-layer bleed hole flow coefficient behavior [microform] / David O. Davis, Marcus Grimes, Mark Schoenenberger.
Microform
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor], 1997]
1997
0 resources
Advanced space propulsion system flowfield modeling [microform] : final report : contract NAS8-40845 / by Sheldon D. Smith.
Microform
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Boundary layer flow control with a One Atmosphere Uniform Glow Discharge Surface Plasma [microform] / J. Reece Roth and Daniel M. Sherman and Stephen P. Wilkinson.
Microform
Reston, Va. : American Institute of Aeronautics and Astronautics ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Boundary-layer receptivity due to distributed surface imperfections of a deterministic or random nature [microform] / Meelan Choudhari.
Microform
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
1992
1 resource
Available online
Concerning the interaction of non-stationary cross-flow vortices in a three-dimensional boundary layer [microform] / Andrew P. Bassom, Philip Hall.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
1990
1 resource
Available online
Numerical simulation of particle-wave interaction in boudary layers [microform] : final report for NAG-1-798 / S. Biringen and G. Danabasaoglu.
Microform
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1991]
1991
1 resource
Available online
On the instability of hypersonic flow past a flat plate [microform] / Nicholas Blackaby, Stephen Cowley, Philip Hall.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
1990
1 resource
Available online
The effects of forcing on a single stream shear layer and its parent boundary layer [microform] / prepared by Richard C. Haw, John F. Foss.
Microform
East Lansing, MI : College of Engineering, Michigan State University, [1990]
1990
1 resource
Available online
The boundary layer on compressor cascade blades [microform] / submitted by Steven Deutsch and William C. Zierke.
Microform
State College, PA : Applied Research Laboratory, The Pennsylvania State University ; [Washington, D.C. : National Aeronautics and Space Administration, 1986]
1986
0 resources
Studies of acoustic effects on a flow boundary layer in air [microform] / F. Mechel and W. Schilz.
Microform
Washington, D.C. : National Aeronautics and Space Administration, [1986]
1986
0 resources
The Upper-branch stability of compressible boundary layer flows [microform] / J.S.B. Gajjar and J.W. Cole.
Microform
[Washington, D.C.] : National Aeronautics and Space Administration ; Cleveland, Ohio : Lewis Research Center, Institute for Computational Mechanics in Propulsion, [1989]
1989
1 resource
Available online
Performance tests for the NASA Ames Research Center 20 cm x 40 cm oscillating wind tunnel [microform] : progress report / William J. Cook and Tim A. Giddings.
Microform
Ames, Iowa : Engineering Research Institute, Iowa State University, [1984]
1984
0 resources
Improved two-dimensional-kinetics computer program [microform] : second quarterly progress report, 1 April 1984 through 30 June 1984 / prepared by Gary R. Nickerson.
Microform
Santa Ana, Calif. : Software and Engineering Associates, Inc. ; [Washington, D.C. : National Aeronautics and Space Administration, 1984?]
1984
0 resources
Boundary layer simulation improvement [microform] : progress report / prepared by Sarat C. Praharaj.
Microform
Huntsville, Ala. : Remtech, inc. ; Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1987]
1987
0 resources
Interaction between Tollmien-Schlichting waves and free-stream disturbances in boundary-layer flows / R. J. Bodonyi.
Microform
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1986]
1986
0 resources