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Effect of pressure gradient on first mode of instability in high-speed boundary layers [microform] / Jamal A. Masad, Yousef H. Zurigat.
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
A phase equation approach to boundary layer instability theory [microform] : Tollmien Schlichting waves / Philip Hall.
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
Effect of nonzero surface admittance on receptivity and stability of compressible boundary layer [microform] / Meelan Choudhari.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Vortex instabilities in 3D boundary layers [microform] : the relationship between Görtler and crossflow vortices / Andrew P. Bassom nad Philip Hall.
Text
Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
1990
0 resources
The inviscid axisymmetric stability of the supersonic flow along a circular cylinder [microform] / Peter W. Duck.
Text
Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
1989
0 resources
Experiments to verify nonparallel stability theory at Virginia Polytechnic Institute and State University, Blacksburg, Virginia [microform] : final report / by William S. Saric.
Text
Tempe, Ariz. : Dept. of Mechanical and Aerospace Engineering, Arizona State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1988]
1988
0 resources
Supersonic laminar flow control research [microform] : semi-annual report #2, July 1994 - December 1994 / C.F. Lo, principal investigator.
Text
Moffett Field, CA : Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Active control of instabilities in laminar boundary-layer flow [microform] / Ronald D. Joslin, Gordon Erlebacher, M. Yousuff Hussaini.
Text
Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994- ]
1994-present
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
Parametric study on laminar flow for finite wings at supersonic speeds [microform] / Joseph Avila Garcia.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Supersonic laminar flow control research [microform] : semiannual report #2 / Dr. C.F. Lo, principal investigator.
Text
Moffett Field, Calif. : Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
On the modulational instability of large amplitude waves in supersonic boundary layers [microform] / Philip Hall, Demetrious T. Papageorgiou.
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
The application to airfoils of a technique for reducing orifice-induced pressure error at high Reynolds numbers [microform] / E.B. Plentovich.
Text
[Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : National Technical Information Service, distributor], 1986.
1986
0 resources
Stability characteristics of a supersonic boundary layer and their relation to the position of the laminar-turbulent transition point [microform] / V.I. Lysenko.
Text
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1987]
1987
0 resources
Non-linear boundary-layer receptivity due to distributed surface roughness [microform] : final report / by principal investigator, Gregory V. Selby, Tahani R. Amer, graduate research assistant.
Text
Norfolk, Va. : Old Dominion University Research Foundation, Dept. of Mechanical Engineering, College of Engineering & Technology ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
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
Supersonic laminar flow control research [microform] : semiannual report #4, July 1995 - December 1995 / Dr. C.F. Lo, principal investigator.
Text
Moffett Field, CA : Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Supersonic laminar flow control research [microform] : semiannual report #4, July 1995-December 1995 / C.F. Lo, principal investigator.
Text
Moffett Field, CA : Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel [microform] / Glen P. Doggett and Ndaona Chokani.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
An approach to the constrained design of natural laminar flow airfoils [microform] : a thesis ... / by Bradford Earl Green.
Text
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
The role of nonlinear critical layers in boundary layer transition [microform] / by M.E. Goldstein.
Text
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
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.
Text
Zhukovsky, Russia : Central Aero-Hydrodynamics Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
A review of hypersonic boundary layer stability experiments in a quiet Mach 6 wind tunnel [microform] / Stephen P. Wilkinson.
Text
Reston, VA : American Institute of Astronautics and Aeronautics ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Distributed-roughness effects on stability and transition in swept-wing boundary layers [microform] : annual technical report ... NASA-Langley cooperative agreement # NCC-1-194 and the Boeing Company contract #ZA0078, during 5/17/96-12/31/96 / submitted by Ruben B. Carrillo, Jr.; Mark S. Reibert; William S. Saric (principal investigator).
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
On the environmental realizability of algebraically growing distrurbances and their relation to Klebanoff modes [microform] / Marvin E. Goldstein, David W. Wundrow.
Text
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, VA : Available from National Technical Information Service, distributor, [1998]
1998
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.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Active control of boundary-layer instabilities [microform] : use of sensors and spectral controller / R.D. Joslin ... [et al.].
Text
Washington, DC : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
A quiet tunnel investigation of hypersonic boundary-layer stability over a cooled, flared cone [microform] : final report / principal investigator, Gregory V. Selby ; submitted by the Old Dominion University Research Foundation.
Text
Norfolk, Va. : Dept. of Mechanical Engineering, College of Engineering & Technology, Old Dominion University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Supersonic laminar flow control research [microform] : final report, July 1994-June 1996 / C.F. Lo, principal investigator.
Text
Tullahoma, TN : University of Tennessee, Space Institute ; Moffett Field, CA : Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Design and predictions for a high-altitude (low-Reynolds-number) aerodynamic flight experiment [microform] / Donald Greer ... [et al.].
Text
Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
1999
0 resources
On the instability of hypersonic flow past a flat plate [microform] / Nicholas Blackaby, Stephen Cowley, 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/LPS60955Effect of suction on controlling the secondary instability of boundary layers [microform] / Nabil M. El-Hady.
Text
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
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS65496Stability of the laminar boundary layer in a streamwise corner [microform] / by William D. Lakin.
Text
Norfolk, Va. : Old Dominion University Research Foundation ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
1984
0 resources
On the stability of an infinite swept attachment line boundary layer [microform] / P. Hall, M. R. Malik, D. I. A. Poll.
Text
Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, [1984]
1984
0 resources
Newton like [microform] : minimal residual methods applied to transonic flow calculations / Yau Shu Wong.
Text
Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, [1984]
1984
0 resources
Feasibility and benefits of laminar flow control on supersonic cruise airplanes [electronic resource] / A.G. Powell, S. Agrawal, T. R. Lacey.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989]
1989
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS113610Feasibility and benefits of laminar flow control on supersonic cruise airplanes [microform] / A.G. Powell, S. Agrawal, T. R. Lacey.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989]
1989
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS113610Wave phenomena in a high Reynolds number compressible boundary layer [microform] / A. Bayliss ... [et al.].
Text
Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, [1985]
1985
0 resources
Delay of transition using forced damping / Reginald J. Exton.
Text
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, November 2014.
2014-11
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo59323Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3 / Robert L. Stallings, Jr., and Milton Lamb.
Text
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
1980-12
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo71443Effects of forebody geometry on subsonic boundary-layer stability / S. S. Dodbele.
Text
[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
1 resource
Available online
https://purl.fdlp.gov/GPO/LPS60902Application of laminar flow control to supersonic transport configurations.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
1990
1 resource
Available online
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