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Subject: "Visualization."
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Langley Research Center
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1.
An implicit method for the calculation of inlet flow fields
Author
Biringen, Sedat
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981.
Location
Library Shelving Facility (LSF) >> NASA CR-3414
Format
Books
2.
Experimental design studies and flow visualization of proportional laminar-flow fluidic amplifiers
Author
Hellbaum, R. F.
Published
Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977.
Location
Library Shelving Facility (LSF) >> NASA TN D-8433
Format
Books
3.
Prediction of vortex shedding from circular and noncircular bodies in subsonic flow
Author
Mendenhall, M. R.
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
Library Shelving Facility (LSF) >> NASA CR-4037
Format
Books
4.
Flow visualization studies of a general research fighter model employing a strake-wing concept at subsonic speeds
Author
Luckring, James M.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1979.
Location
SML, Microform (Non-Circulating) >> NAS 1.15:80057
Library Shelving Facility (LSF) >> NASA TM-80057
Format
Books / Microforms
5.
Digital enhancement of flow field images
Author
Kudlinski, Robert A.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1988.
Location
Library Shelving Facility (LSF) >> NAS 1.60:2770
Format
Books
6.
Prediction of vortex shedding from circular and noncircular bodies in supersonic flow
Author
Mendenhall, M. R.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984.
Location
Library Shelving Facility (LSF) >> NASA CR-3754
Format
Books
7.
A simplified holographic-interferometry technique for real-time flow visualization and analysis
Author
Long, Sheila Ann T.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974.
Location
Library Shelving Facility (LSF) >> NASA TN D-7421
Format
Books
8.
Aerodynamic and flow-visualization studies of variations in the geometry of irregular planform wings at a Mach number of 20.3
Author
Stone, David R. (David Ray)
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974.
Location
Library Shelving Facility (LSF) >> NASA TN D-7650
Format
Books
9.
A study of prediction methods for the high angle-of-attack aerodynamics of straight wings and fighter aircraft
Author
McMillan, Oden J.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1984.
Location
Library Shelving Facility (LSF) >> NASA CR-3764
Format
Books
10.
Pressure data for four analytically defined arrow wings in supersonic flow
Author
Townsend, James C. (James Courtland), 1938-
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1980.
Location
Library Shelving Facility (LSF) >> NASA TM-81835
SML, Microform (Non-Circulating) >> NAS 1.15:81835
Format
Books / Microforms
11.
Diffusion model study in chemically reacting air couette flow with hydrogen injection
Author
Graves, Randoph A., Jr
Published
Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1970.
Location
Library Shelving Facility (LSF) >> NASA TR R-349
Format
Books
12.
Surface pressure data on a series of analytic forebodies at Mach numbers from 1.70 to 4.50 and combined angles of attack and sideslip
Published
Washington, D.C.: National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1979.
Location
Library Shelving Facility (LSF) >> NASA TM-80062
SML, Microform (Non-Circulating) >> NAS 1.15:80062
Format
Books / Microforms
13.
TWINTN4 : a program for transonic four-wall interference assessment in two-dimensional wind tunnels
Author
Kemp, William B.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1984.
Location
Library Shelving Facility (LSF) >> NASA CR-3777
Format
Books
14.
Finite element analysis and computer graphics visualization of flow around pitching and plunging airfoils
Author
Bratanow, Theodore
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973.
Location
Library Shelving Facility (LSF) >> NASA CR-2249
Format
Books
15.
Spectroscopic analysis of electron-beam-induced fluorescence in hypersonic helium flow
Author
Hillard, Mervin E., Jr
Published
Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970.
Location
Library Shelving Facility (LSF) >> NASA TN D-6005
Format
Books
16.
Wind-tunnel investigation of a simulated gunship helicopter engine-exhaust-windstream interaction
Author
Wilson, John C.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974.
Location
Library Shelving Facility (LSF) >> NASA TM X-3161
Format
Books
17.
Laser Doppler velocity measurements of swirling flows with upstream influence
Author
Orloff, Kenneth L.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973.
Location
Library Shelving Facility (LSF) >> NASA CR-2284
Format
Books
18.
Influence of upstream flow discontinuities on the acoustic power radiated by a model air jet
Author
Gordon, Colin G.
Published
Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1967.
Location
Library Shelving Facility (LSF) >> NASA CR-679
Format
Books
19.
Measurements of flow angles in vicinity of two lifting forebody configurations at a Mach number of 2.01
Author
Morris, Odell A.
Published
Washington, D.C. : National Aeronautics and Space Administration, 1963.
Location
Library Shelving Facility (LSF) >> NASA TN D-1640
Format
Books
20.
Vapor-screen flow-visualization experiments in the NASA Langley 0.3-m transonic cryogenic tunnel
Author
Selby, Gregory V. (Gregory Vincent)
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
Library Shelving Facility (LSF) >> NASA CR-3984
Format
Books
21.
Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8t̊o 90 ̊
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983-
Location
Library Shelving Facility (LSF) >> NASA CR-3246
Format
Books
22.
Aerodynamic and flow-visualization studies of two delta-wing entry vehicles at a Mach number of 20.3
Author
Arrington, James P.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973.
Location
Library Shelving Facility (LSF) >> NASA TN D-7282
Format
Books
23.
Real-helium hypersonic flow parameters for pressures to 3600 atmospheres and temperatures to 15 000° K
Author
Miller, Charles G. (Charles George), 1940-
Published
Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 2215], 1968.
Location
Library Shelving Facility (LSF) >> NASA TN D-4869
Format
Books
24.
Fixed-base simulator study of the effect of time delays in visual cues on pilot tracking performance
Author
Queijo, M. J.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975.
Location
Library Shelving Facility (LSF) >> NASA TN D-8001
Format
Books
25.
Visual aspects of a full-size pilot-controlled simulation of the Gemini-Agena docking
Published
Washington, D.C. : National Aeronautics and Space Administration : For sale by the Office of Technical Services, Dept. of Commerce, [1965]
Location
Library Shelving Facility (LSF) >> NASA TN D-2632
Format
Books