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Wind tunnels > Flow visualization

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Online Results (33)
1.
Fiber-optic-based laser vapor screen flow visualization sysytem for aerodynamic research in larger scale subsonic and transonic wind tunnels
Author
Erickson, Gary E.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
Location
SML, Microform (Non-Circulating) >> NAS 1.15:4514
Format
Books / Microforms
2.
A supersonic tunnel for laser and flow-seeding techniques
Author
Bruckner, Robert J.
Published
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
Location
SML, Microform (Non-Circulating) >> NAS 1.15:106588
Format
Books / Microforms
3.
Supersonic flow visualization of a nacelle in close proximity to a simulated wing
Author
Biber, Kasim
Published
Wichita, Kan. : National Institute for Aviation Research, Wichita State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993]
Location
SML, Microform (Non-Circulating) >> NAS 1.26:194675
Format
Books / Microforms
4.
Experimental parametric study of jet vortex generators for flow separation control
Author
Selby, Gregory V. (Gregory Vincent)
Published
Norfolk, Va. : Old Dominion University Research Foundation, [1991]
Online
http://purl.access.gpo.gov/GPO/LPS65621
Location
SML, Microform (Non-Circulating) >> NAS 1.26:187836
Format
Books / Microforms
5.
Visualization of leading edge vortices on a series of flat plate delta wings
Author
Payne, Francis M.
Published
[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], 1991.
Location
SML, Microform (Non-Circulating) >> NAS 1.26:4320
Format
Books / Microforms
6.
Visualization of leading edge vortices on a series of flat plate delta wings
Author
Payne, Francis M.
Published
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, 1991.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
7.
A laser-sheet flow visualization technique for the large wind tunnels of the National Full-Scale Aerodynamics Complex
Author
Reinath, M. S.
Published
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
Location
SML, Microform (Non-Circulating) >> NAS 1.15:102793
Format
Books / Microforms
8.
Effect of aspect ratio on sidewall boundary-layer influence in two-dimensional airfoil testing
Author
Murthy, A. V.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Location
Library Shelving Facility (LSF) >> NASA CR-4008
Format
Books
9.
Improvement in the quality of flow visualization in the Langley 0.3-meter transonic cryogenic tunnel
Author
Snow, W. L.
Published
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1986.
Location
SML, Microform (Non-Circulating) >> NAS 1.15:87730
Format
Books / Microforms
10.
Improvement in the quality of flow visualization in the Langley 0.3-meter transonic cryogenic tunnel
Author
Snow, W. L.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online