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Control of flow separation : energy conservation, operational efficiency, and safety / by Paul K. Chang.
Text
Washington : Hemisphere Pub. Cor., c1976. distributed by McGraw-Hill, [1975]
1975
1 item
| Format | Call number | Item location |
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| FormatText | Call numberJSE 77-267 | Item locationOffsite |
Boundary layer and flow control, its principles and application.
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New York, Pergamon Press, 1961.
1961
2 items
| Format | Call number | Item location |
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| FormatText | Call numberPCP (Lachmann, G. Boundary layer and flow control) v. 2 (1961) | Item locationOffsite |
| Format | Call number | Item location |
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| FormatText | Call numberPCP (Lachmann, G. Boundary layer and flow control) v. 1 (1961) | Item locationOffsite |
F-16XL-2 supersonic laminar flow control flight test experiment [microform] / Scott G. Anders and Michael C. Fischer.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information ; Springfield, VA : National Technical Information Service [distributor, 1999]
1999
0 resources
Subsonic investigation of a leading-edge boundary layer cont[r]ol suction system on a high-speed civil transport configuration [microform] / Bryan A. Campbell ... [et al.].
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information ; Springfield, VA : National Technical Information Service [distributor, 1999]
1999
0 resources
Application of computational fluid dynamics to the study of vortex flow control for the management of inlet distortion [microform] / Bernhard H. Anderson and James Gibb.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1992]
1992
0 resources
Adaptive nonlinear polynomial neural networks for control of boundary layer/structural interaction [microform] / B. Eugene Parker, Jr. ... [et al.].
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1993]
1993
0 resources
Vortex boundary-layer interactions, data report [microform] : semiannual status report on research grant no. NAGW-581, period 1 March 1985 - 31 August 1985 / P. Bradshaw, principal investigator.
Text
London : Imperial College of Science and Technology, Department of Technology ; [Springfield, Va. : For sale by the National Technical Information Service, 1985]
1985
0 resources
Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction [microform] : final report / by H.T. Nagamatsu and R. Dyer.
Text
[Hampton, Va.? : National Aeronautics and Space Administration, Langley Research Center, 1984]
1984
0 resources
Acoustic receptivity of compressible boundary layers [microform] : receptivity via surface-temperature variations / Meelan Choudhari.
Text
Hampton, Va. : National Aeronautics and Space Administration, 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
Analysis and evaluation of an integrated laminar flow control propulsion system [microform] : final technical report / Theo G. Keith, Jr., Kenneth J. De Witt.
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[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993]
1993
0 resources
Analysis of the leading edge effects on the boundary layer transition [microform] : technical report, March 1, 1984 - August 31, 1990 / submitted by Pao-Liu Chow, principal investigator.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1990]
1990
0 resources
1989 high-speed civil transport studies [microform] / HSCT Concept Development Group, Advanced Commercial Programs, Douglas Aircraft Company.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
1991
0 resources
The NASA Langley laminar-flow-control experiment on a swept supercritical airfoil [microform] : basic results for slotted configuration / Charles D. Harris ... [et al.].
Text
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1989.
1989
0 resources
Performance of the active sidewall boundary-layer removal system for the Langley 0.3-meter transonic cryogenic tunnel [microform] / S. Balakrishna, W. Allen Kilgore, and A.V. Murthy.
Text
Hampton, Va. : National Aeronautics and Space Administration, 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.
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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
Control of unsteady separated flow associated with the dynamic stall of airfoils [microform] / M.C. Wilder.
Text
San Jose, CA : MCAT Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Numerical simulation of the SOFIA flowfield [microform] / Stephen P. Klotz.
Text
San Jose, CA : MCAT Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
On supersonic-inlet boundary-layer bleed flow [microform] / Gary J. Harloff and Gregory E. Smith.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
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
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
Approximation of discrete-time LQG compensators for distributed systems with boundary input and unbounded measurement [microform] / J.S. Gibson, I.G. Rosen.
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Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1987]
1987
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
Stability and control of compressible flows over a surface with concave-convex curvature [microform] / Lucio Maestrello ... [et al.].
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
Evaluation of laminar flow control systems concepts for subsonic commercial transport aircraft [microform] / McDonnel Douglas Corporation, Douglas Aircraft Company.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1983]
1983
0 resources
Application of hybrid laminar flow control to global range military transport aircraft [microform] / Roy H. Lange.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
1988
0 resources
LFC leading edge glove flight [microform] : aircraft modification design, test article development, and systems integration / F.R. Etchberger, et al.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1983]
1983
0 resources
Effect of aspect ratio on sidewall boundary-layer influence in two-dimensional airfoil testing [microform] / A.V. Murthy.
Text
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : National Technical Information Service, distributor], 1986.
1986
0 resources
Control of unsteady separated flow associated with the dynamic stall of airfoils [microform] : final report, 95-09 / M.C. Wilder.
Text
San Jose, CA : MCAT Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Numerical simulation of supersonic flow using a new analytical bleed boundary condition [microform] / G.J. Harloff and G.E. Smith.
Text
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Boundary layer transition studies [microform] : November 1990 to February 1995 / Jonathan H. Watmuff.
Text
San Jose, CA : MCAT Institute ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
A self-contained, automated methodology for optimal flow control validated for transition delay [microform] / Ronald D. Joslin ... [et al.].
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
Flow characteristics in boundary layer bleed slots with plenum [microform] / A. Hamed, J.J. Yeuan and J.D. Jun.
Text
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 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
Hybrid laminar flow control experiments in the NASA - Ames, 11-foot tunnel [microform] : final report / submitted by William S. Saric.
Text
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction [microform] : final report on NASA grant NAG 1-1471 for the period 01/09/93 through 01/01/95 / David S. Dolling and J.W. Barter.
Text
Austin, Tex. : Center for Aerodynamics Research, Dept. of Aerospace Engineering & Engineering Mechanics, University of Texas at Austin ; [Washington, DC : National Aeronautics and Space Administration ; 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
Experimental investigation of crossing shock wave-turbulent boundary layer-bleed interaction [microform] / Hyun D. Kim, Warren R. Hingst, and David O. Davis.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Renormalization Group (RG) in turbulence [microform] : historical and comparative perspective / Ye Zhou, W. David McComb, George Vahala.
Text
Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Optimum suction distribution for transition control [microform] / P. Balakumar, P. Hall.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
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.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Porous and microporous honeycomb composites as potential boundary-layer bleed materials [microform] / D.O. Davis and B.P. Willis, M. Schoenenberger.
Text
[Washington, D.C. : National Aeronautics and Space Administration ; 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.
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
Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction [microform] / D.O. Davis, B.P. Willis, and W.R. Hingst.
Text
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
1998
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
Overview of laminar flow control [microform] / Ronald D. Joslin.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
1998
0 resources
High Reynolds number hybrid laminar flow control (HLFC) flight experiment. IV, Suction system design and manufacture [microform] / Boeing Commercial Airplane Group.
Text
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. III, Leading edge design, fabrication, and installation [microform] / Boeing Commercial Airplane Group.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
1999
0 resources
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