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Validation of the RPLUS3D code for supersonic inlet applications involving three-dimensional shock wave boundary layer interactions [microform] / Kamlesh Kapoor, Bernard H. Anderson.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Computation of three-dimensional compressible boundary-layers to fourth-order accuracy on wings and fuselages [microform] / Venkit Iyer.
Text
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor], 1990.
1990
0 resources
Assessment of a 3-D boundary layer analysis to predict heat transfer and flow field in a turbine passage [microform] / by O.L. Anderson.
Text
East Hartford, Conn. : United Technologies Research Center ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1985]
1985
0 resources
User's manual for three dimensional boundary layer (BL3-D) code [microform] / by O.L. Anderson, B. Caplin.
Text
East Hartford, Conn. : United Technologies Research Center ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1985]
1985
0 resources
A spectrally accurate boundary-layer code for infinite swept wings [microform] / C. David Pruett.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1994
0 resources
Effect of crossflow on Görtler instability in incompressible boundary layers [microform] / Y.H. Zurigat, M.R. Malik.
Text
Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Wave interactions in a three-dimensional attachment line boundary layer [microform] / Phillp Hall, Sharon O. MacKerrell.
Text
Hampton, VA : NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
1988
0 resources
Nonlinear stability of non-stationary cross-flow vortices in compressible boundary layers [microform] / J.S.B. Gajjar.
Text
[Cleveland, Ohio] : Institute for Computational Mechanics in Propulsion, NASA Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Incipient transition phenomena in compressible flow over a flat plate [microform] / G. Erlebacker, M.Y. Hussaini.
Text
Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
1986
0 resources
Multiple scales approach to weakly nonparallel and curvature effects [microform] : details for the novice / Bart A. Singer and Meelan Choudhari.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
On the nonlinear evolution of a stationary cross-flow vortex in a fully three-dimensional boundary layer flow [microform] / J.S.B. Gajjar.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
The nonlinear evolution of inviscid Gortler vortices in three-dimensional boundary layers [microform] / Nicholas Blackaby, Andrew Dando, Philip Hall.
Text
Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Simulation of crossflow instability on a supersonic highly swept wing [microform] / C. David Pruett.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
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.
Text
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
Effect of surface waviness on transition in three-dimensional boundary-layer flow [microform] / Jamal A. Masad.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Direct numerical simulation of evolution and control of linear and nonlinear disturbances in three-dimensional attachment-line boundary layers [microform] / Ronald D. Joslin.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Spanwise spacing effects on the initial structure and decay of axial vortices [microform] : under contract NAS3-27377 / B.J. Wendt and B.A. Reichert.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
On the stability of three-dimensional boundary layers [microform] / Erik Janke, Ponnampalam Balakumar.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999- ]
1999-present
0 resources
Direct harmonic linear Navier-Stokes methods for efficient simulation of wave packets [microform] / C.L. Streett.
Text
Reston, Va. : American Institute of Aeronautics and Astronautics ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Concerning the interaction of non-stationary cross-flow vortices in a three-dimensional boundary layer [microform] / Andrew P. Bassom, Philip Hall.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
1990
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS60957Three-dimensional effects on airfoils [microform] / J.P. Chevallier.
Text
Washington, D.C. : National Aeronautics and Space Administration, [1983]
1983
0 resources
Three-dimensional boundary layer analysis program "Blay" and its application [microform] / Ken-ichi Matsuno and Tomiko Ishiguro.
Text
Washington, D.C. : National Aeronautics and Space Administration, [1986]
1986
0 resources
Mean veoIocity and turbulence measurements in a 90⁰ curved duct with thin inlet boundary layer [microform] : final report / R. A. Crawford ... [et al.].
Text
Tullahoma, Tenn. : University of Tennessee Space Institute, [1985]
1985
0 resources
Mean velocity and turbulence measurements in a 90° curved duct with thin inlet boundary layer : final report / R. A. Crawford ... [and others].
Text
Tullahoma, Tenn. : University of Tennessee Space Institute ; [Cleveland, Ohio] : NASA Lewis Research Center, [1985]
1985
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo22000Calculation of laminar heating rates on three-dimensional configurations using the axisymmetric analogue / H. Harris Hamilton II.
Text
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, September1980.
1980-9
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo70978No results found from Digital Research Books Beta
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