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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
Fully nonlinear Görtler vortices in constricted channel flows and their effect on the onset of separation [microform] / James P. Denler, Philip Hall.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
1992
0 resources
Cryogenic tunnel pressure measurements on a supercritical airfoil for several shock buffet conditions [microform] / Robert E. Bartels and John W. Edwards.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
High Reynolds number effects on multi-hole probes and hot wire anemometers [microform] / N. Ramachandran ... [et al.].
Microform
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
A note on kinetic energy, dissipation and enstrophy [microform] / Jie-Zhi Wu, Ye Zhou, Meng Fan.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Multigrid strategies for viscous flow solvers on anisotropic unstructured meshes [microform] / Dimitri J. Mavriplis.
Microform
Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
1998
0 resources
Directional agglomeration multigrid techniques for high-Reynolds number viscous flows [microform] / Dimitri J. Mavriplis.
Microform
Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
1998
0 resources
Computation of separated and unsteady flows with one- and two-equation turbulence models [microform] : 32nd Aerospace Sciences meeting & exhibit, January 10-13, 1994/Reno, NV / J.A. Ekaterinaris and F.R. Menter.
Microform
Washington, D.C. : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet [microform] / Michael K. Ponton, Lawrence S. Ukeiley, Sang W. Lee.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
1999
0 resources
High Reynolds number hybrid laminar flow control (HLFC) flight experiment. IV, Suction system design and manufacture [microform] / Boeing Commercial Airplane Group.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
1999
0 resources
High Reynolds number hybrid laminar flow control (HLFC) flight experiment. II, Aerodynamic design [microform] / Boeing Commercial Airplane Group.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
1999
0 resources
Directional agglomeration multigrid techniques for high Reynolds number viscous flow solvers [microform] / D.J. Mavriplis.
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
Assessment of an Euler-interacting boundary layer method using high Reynolds number transonic transport flight data [microform] / Daryl L. Bonhaus and Dal V. Maddalon.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
1998
0 resources
Algebraic turbulence modeling for unstructured and adaptive meshes [microform] / Dimitri J. Mavriplis.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
1990
1 resource
Available online
The stability of two-dimensional wakes and shear-layers at high Mach numbers [microform] / D.T. Papageorgiou.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
1990
1 resource
Available online
Optimization of an advanced design three-element airfoil at high reynolds numbers / J.C. Lin, C.J. Dominik.
Microform
[Washington, D.C.] : National Aeronautics and Space Administration, [1995]
1995
0 resources