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Analysis of aerospike plume induced base-heating environment [microform] / T.-S. Wang.
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
Low speed analysis of mission adaptive flaps on a high speed civil transport configuration [microform] / Victor R. Lessard.
Microform
Hampton, Va. : National Aeronautics and Space Administration, 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
Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil [microform] / Dale Ashby.
Microform
[Stanford, Calif.] : Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center : Joint Institute for Aeronautics and Acoustics, Stanford University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Laser anemometer measurements of the flow field in a 4:1 pressure ratio centrifugal impeller [microform] / G.J. Skoch ... [et al.].
Microform
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Experimental study of saddle point of attachment in laminar juncture flow [microform] / Michael D. Coon and Murray Tobak.
Microform
Washington, DC : American Institute of Aeronautics and Astronautics, Inc. : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Study of boundary layer development in a two-stage low-pressure turbine [microform] / Daniel J. Dorney ... [et al.].
Microform
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
1999
0 resources
Experimental study of boundary layer behavior in a simulated low pressure turbine [microform] / Rickey J. Shyne.
Microform
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
The three dimensional flow field at the exit of an axial-flow turbine rotor [microform] / B. Lakshminarayana, D. Ristic, and S. Chu.
Microform
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, VA : National Technical Information Service [distributor, 1998]
1998
0 resources
Effects of convoluted divergent flap contouring on the performance of a fixed-geometry nonaxisymmetric exhaust nozzle [microform] / Scott C. Asbury and Craig A. Hunter.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
1999
0 resources
Implementation and validation of the Chien k-[epsilon] turbulence model in the Wind Navier-Stokes code [microform] / Dennis A. Yoder and Nicholas J. Georgiadis.
Microform
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
1999
0 resources
Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method [microform] : EUROMECH-Colloquium 349, simulation of fluid-structure interaction in aeronautics, Göttingen, Germany, September 16-18, 1996 / John W. Edwards.
Microform
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Investigation of flow separation in a transonic-fan linear cascade using visualization methods [microform] / Jan Lepicovsky ... [et al.].
Microform
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : National Technical Information Service, distributor, [2000]
2000
0 resources
Closed-loop separation control using oscillatory flow excitation [microform] / Brian G. Allan ... [et al.] ; [prepared for ... under contract NAS1-97046].
Microform
Hampton, Va. : ICASE, National Aeronautics and Science Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2000]
2000
0 resources
Enhanced design of turbo-jet LPT by separation control using phased plasma actuators [microform] / Thomas C. Corke and Flint O. Thomas.
Microform
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Administration ; Springfield, VA : National Technical Information Service [distributor, 2003]
2003
1 resource
Available online
Demonstration of separation delay with glow-discharge plasma actuators [microform] / Lennart S. Hultgren and David E. Ashpis.
Microform
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, Md. : Available from the NASA Center for Aerospace Information ; Springfield, VA : National Technical Information Service [distributor, 2003]
2003
1 resource
Available online
Some observations on transitory stall in conical diffusers [microform] / K.B.M.Q. Zaman and M.D. Dahl.
Microform
Cleveland, Ohio : Lewis Research Center, [1989]
1989
1 resource
Available online
Flow separation in shock wave boundary layer interactions at hypersonic speeds [microform] / A. Hamed.
Microform
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
Jet vortex generators for turbulent flow separation control [microform] / by Gregory Selby.
Microform
Norfolk, Va. : Old Dominion University Research Foundation ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
1990
1 resource
Available online
Numerical approach for the aerodynamic analysis of airfoils with laminar separation [microform] / prepared by David W. Halt and Dean R. Bristow.
Microform
St. Louis, Mo. : McDonnel Douglas Corporation, McDonnel Aircraft Company ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
1985
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