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Transonic wind tunnels

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Online Results (123)
1.
Feasibility of Rayleigh scattering flow diagnostics in the National Transonic Facility
Author
Herring, Gregory C.
Published
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, September 2015.
Online
http://purl.fdlp.gov/GPO/gpo66100
Location
Yale Internet Resource >> None
Format
Books / Online
2.
11 foot Unitary Plan tunnel facility optical improvement large window analysis
Author
Hawke, Veronica M.
Published
Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, February 2015.
Online
http://purl.fdlp.gov/GPO/gpo57082
Location
Yale Internet Resource >> None
Format
Books / Online
3.
Pressure- and temperature-sensitive paint at 0.3-m transonic cryogenic tunnel
Author
Watkins, A. Neal
Published
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, September 2015.
Online
http://purl.fdlp.gov/GPO/gpo64042
Location
Yale Internet Resource >> None
Format
Books / Online
4.
Measuring global surface pressures on a circulation control concept using pressure sensitive paint
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012]
Online
http://purl.fdlp.gov/GPO/gpo30920
Location
Yale Internet Resource >> None
Format
Books / Online
5.
Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics Tunnel
Author
Schuster, D. M. (David M.)
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information (CASI), [2001]
Online
Adobe Acrobat Reader required
Location
SML, Microform (Non-Circulating) >> NAS 1.15:210828
Format
Books / Microforms
6.
Aerodynamic measurements on a large splitter plate for the NASA Langley Transonic Dynamics Tunnel
Author
Schuster, D. M. (David M.)
Published
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, March 2001.
Online
http://purl.access.gpo.gov/GPO/LPS22955
Location
Yale Internet Resource >> None
Format
Books / Online
7.
Cryogenic pressure calibrator for wide temperature electronically scanned (ESP) pressure modules
Author
Faulcon, Nettie D.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information (CASI), [2001]
Online
Adobe Acrobat Reader required
Location
SML, Microform (Non-Circulating) >> NAS 1.15:211031
Format
Books / Microforms
8.
A historical overview of Aeroelasticity Branch and Transonic Dynamics Tunnel contributions to rotorcraft technology and development
Author
Yeager, William T.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information (CASI), [2001]
Online
Adobe Acrobat Reader required
Location
SML, Microform (Non-Circulating) >> NAS 1.15:211054
Format
Books / Microforms
9.
Langley 16-ft. Transonic Tunnel Pressure Sensitive Paint System
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information (CASI), [2001]
Online
Adobe Acrobat Reader required
Location
SML, Microform (Non-Circulating) >> NAS 1.15:211017
Format
Books / Microforms
10.
Sidewall Mach number distributions for the NASA Langley Transonic Dynamics Tunnel
Author
Florance, James R.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information (CASI), [2001]
Online
Adobe Acrobat Reader required
Location
SML, Microform (Non-Circulating) >> NAS 1.15:211019
Format
Books / Microforms
11.
Development of a large field of view shadowgraph system for a 16 ft. transonic wind tunnel
Author
Talley, Michael A.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information (CASI), [2000]
Online
Adobe Acrobat Reader required
Location
SML, Microform (Non-Circulating) >> NAS 1.15:210311
Format
Books / Microforms
12.
Control of the NASA Langley 16-foot transonic tunnel with the self-organizing feature map
Author
Motter, Mark A.
Published
[Gainville, Fla.] : University of Florida ; [Washington, D.C.] : [National Aeronautics and Space Administration], 1998.
Online
https://purl.fdlp.gov/GPO/gpo177169
Location
Yale Internet Resource >> None
Format
Books / Online
13.
Cryogenic tunnel pressure measurements on a supercritical airfoil for several shock buffet conditions
Author
Bartels, Robert E.
Published
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, September 1997.
Online
http://purl.fdlp.gov/GPO/gpo75869
Location
Yale Internet Resource >> None
Format
Books / Online
14.
Performance and vibratory loads data from a wind-tunnel test of a model helicopter main-rotor blade with a paddle-type tip
Author
Yeager, William T.
Published
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, May 1997.
Online
http://purl.fdlp.gov/GPO/gpo65467
Location
Yale Internet Resource >> None
Format
Books / Online
15.
Finite element analysis of a NASA National Transonic Facility wind tunnel balance
Author
Lindell, Michael C.
Published
Hampton, Virginia : NASA, NASA Langley Research Center, [1996]
Online
http://purl.fdlp.gov/GPO/gpo78880
Location
Yale Internet Resource >> None
Format
Books / Online
16.
Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf
Author
Lamb, Milton
Published
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, September 1996.
Online
http://purl.fdlp.gov/GPO/gpo65363
Location
Yale Internet Resource >> None
Format
Books / Online
17.
The NASA Langley 16-foot transonic tunnel historical overview, facility description, calibration, flow characteristics, and test capabilities
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
Online
http://purl.access.gpo.gov/GPO/LPS54050
Location
SML, Microform (Non-Circulating) >> NAS 1.60:3521
Format
Books / Microforms
18.
Experimental studies of transonic flow field near a longitudinally slotted wind tunnel wall
Author
Everhart, Joel L.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
Online
http://purl.access.gpo.gov/GPO/LPS60769
Location
SML, Microform (Non-Circulating) >> NAS 1.60:3392
Format
Books / Microforms
19.
Experimental uncertainty and drag measurements in the national transonic facility
Author
Batill, Stephen M.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1994.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
20.
Analysis of fluctuating static pressure measurements in a large high Reynolds number transonic cryogenic wind tunnel
Author
Igoe, William B.
Published
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
Location
SML, Microform (Non-Circulating) >> NAS 1.15:108722
Format
Books / Microforms
21.
Characteristics of vertical and lateral tunnel turbulence measured in air in the Langley Transonic Dynamics Tunnel
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
Location
SML, Microform (Non-Circulating) >> NAS 1.15:107734
Format
Books / Microforms
22.
A feasibility study of using Langley 0.3-m Transonic Cryogenic Tunnel sidewall boundary-layer removable system for heavy gas testing
Author
Murthy, A. V.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
Location
SML, Microform (Non-Circulating) >> NAS 1.26:191438
Format
Books / Microforms
23.
NASA Lewis 8- by 6-foot supersonic wind tunnel user manual
Author
Soeder, Ronald H.
Published
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
Location
SML, Microform (Non-Circulating) >> NAS 1.15:105771
Format
Books / Microforms
24.
Wall interference and boundary simulation in a transonic wind with a discretely slotted test section
Author
Al-Saadi, Jassim A.
Published
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1993.
Location
SML, Microform (Non-Circulating) >> NAS 1.60:3334
Format
Books / Microforms
25.
Comparison of a two-dimensional adaptive-wall technique with analytical wall interference correction techniques
Author
Mineck, Raymond E.
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
26.
Data reduction formulas for the 16-foot transonic tunnel NASA Langley Research Center
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
Location
SML, Microform (Non-Circulating) >> NAS 1.15:107646
Format
Books / Microforms
27.
Experimental study of a generic high-speed civil transport
Author
Belton, Pamela S.
Published
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1992.
Location
SML, Microform (Non-Circulating) >> NAS 1.15:4382
Format
Books / Microforms
28.
Experimental study of a generic high speed civil transport-tabulated data
Author
Belton, Pamela S.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
Location
SML, Microform (Non-Circulating) >> NAS 1.26:104216
Format
Books / Microforms
29.
Further buffeting tests in a cryogenic wind tunnel
Author
Mabey, Dennis G.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
Location
SML, Microform (Non-Circulating) >> NAS 1.15:107621
Format
Books / Microforms
30.
Further investigations of the aeroelastic behavior of the AFW wind-tunnel model using transonic small disturbance theory
Author
Silva, Walter A.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
Location
SML, Microform (Non-Circulating) >> NAS 1.15:107576
Format
Books / Microforms
31.
Modifications to Langley 0.3-m TCT adaptive wall software for heavy gas test medium. Phase 1 studies
Author
Murthy, A. V.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1992]
Online
http://purl.access.gpo.gov/GPO/LPS125650
Location
Yale Internet Resource >> None
Format
Books / Online
32.
Results for the hybrid laminar flow control experiment conducted in the NASA Langley 3-FT transonic pressure tunnel on a 7-ft chord model
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
Location
SML, Microform (Non-Circulating) >> NAS 1.15:107582
Format
Books / Microforms
33.
User guide for WAICX a transonic wind-tunnel wall interference assessment and correction procedure for the NTF
Author
Garriz, Javier A.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
Location
SML, Microform (Non-Circulating) >> NAS 1.15:104168
Format
Books / Microforms
34.
Investigation of the aeroelastic stability of the AFW wind-tunnel model using CAP-TSD
Author
Silva, Walter A.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
Location
SML, Microform (Non-Circulating) >> NAS 1.15:104142
Format
Books / Microforms
35.
Mass flux similarity for slotted transonic-wind-tunnel walls
Author
Everhart, Joel L.
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; Springfield, Va. : For sale by the National Technical Information Service, 1991.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
36.
Mass flux similarity for slotted transonic-wind-tunnel walls
Author
Everhart, Joel L.
Published
[Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1991.
Location
SML, Microform (Non-Circulating) >> NAS 1.15:4281
Format
Books / Microforms
37.
The NASA Langley Research Center 0.3-meter Transonic Cryogenic Tunnel microcomputer Controller source code
Author
Kilgore, W. Allen
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
Location
SML, Microform (Non-Circulating) >> NAS 1.26:189556
Format
Books / Microforms
38.
Slotted-wall flow-field measurements in a transonic wind tunnel
Author
Everhart, Joel L.
Published
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1991.
Location
SML, Microform (Non-Circulating) >> NAS 1.15:4280
Format
Books / Microforms
39.
A study of residual interference effects in adaptive wall testing of a 7-inch chord CAST-10-2/DOA 2 airfoil model
Author
Murthy, A. V.
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; Springfield, Va. : For sale by the National Technical Information Service, 1991.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
40.
A study of residual interference effects in adaptive wall testing of a 7-inch chord CAST-10-2/DOA 2 airfoil model
Author
Murthy, A. V.
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
Location
SML, Microform (Non-Circulating) >> NAS 1.26:4390
Format
Books / Microforms
41.
Wall-interference assessment and corrections for transonic NACA 0012 airfoil data from various wind tunnels
Author
Green, Lawrence L. (Lawrence Lee)
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
42.
Calibration of the 13- by 13-inch adaptive wall test section for the Langley 0.3-Meter Transonic Cryogenic Tunnel
Author
Mineck, Raymond E.
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], 1990.
Location
SML, Microform (Non-Circulating) >> NAS 1.60:3049
Format
Books / Microforms
43.
Calibration of the 13- by 13-inch adaptive wall test section for the Langley O.3-meter transonic cryogenic tunnel
Author
Mineck, Raymond E.
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, 1990.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
44.
Data quality analysis at the National Transonic Facility
Author
Stewart, Pamela N.
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, 1990.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
45.
Data quality analysis at the National Transonic Facility
Author
Stewart, Pamela N.
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, [1990]
Online
http://purl.access.gpo.gov/GPO/LPS65497
Location
SML, Microform (Non-Circulating) >> NAS 1.26:4303
Format
Books / Microforms
46.
High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions
Author
Chu, Julio
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], 1990.
Location
SML, Microform (Non-Circulating) >> NAS 1.15:4227
Format
Books / Microforms
47.
High Reynolds number test of the Boeing TR77 airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
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], 1990.
Location
SML, Microform (Non-Circulating) >> NAS 1.15:4189
Format
Books / Microforms
48.
Realtime multi-plot graphics system
Author
Shipkowski, Michael S.
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, 1990.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
49.
Transonic wind tunnel test of a 14% thick oblique wing
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 1.15:102230
Format
Books / Microforms
50.
Hardware and operating features of the adaptive wall test section for the Langley 0.3-meter transonic cryogenic tunnel
Author
Mineck, Raymond E.
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, 1989.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online