Clear Search

Books+ Search Results

Format: Is
Is Is Not
Online
Subject with Hierarchy: Is
Is Is Not
Transonic wind tunnels

Advanced Search

Basic Search
Help
Add a row
Reset

Limit results by

Remove Online Limit
Viewing Online Items
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 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
6.
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
7.
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
8.
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
9.
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
10.
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
11.
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
12.
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
13.
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
14.
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
15.
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
16.
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
17.
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
18.
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
19.
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
20.
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
21.
Adaptive wall technology for minimization of wall interferences in transonic wind tunnels
Author
Wolf, Stephen W. D.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
22.
Modifications to the Langley 8-foot transonic pressure tunnel for the laminar flow control experiment
Author
Harris, Charles D., 1952-
Published
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Division, May 1988.
Online
http://purl.fdlp.gov/GPO/gpo76274
Location
Yale Internet Resource >> None
Format
Books / Online
23.
Two-dimensional aerodynamic characteristics of the OLS/TAAT airfoil
Author
Watts, Michael E.
Published
[Washington, D.C.?] : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Online
https://purl.fdlp.gov/GPO/gpo92967
Location
Yale Internet Resource >> None
Format
Books / Online
24.
Design study of advanced model support systems for the National Transonic Facility
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1987]
Online
http://purl.fdlp.gov/GPO/gpo33848
Location
Yale Internet Resource >> None
Format
Books / Online
25.
Integration effects of D-shaped, underwing, aft-mounted, separate-flow, flow-through nacelles on a high-wing transport
Author
Lamb, Milton
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, November 1987.
Online
http://purl.fdlp.gov/GPO/gpo76181
Location
Yale Internet Resource >> None
Format
Books / Online
26.
The application to airfoils of a technique for reducing orifice-induced pressure error at high Reynolds numbers
Author
Plentovich, Elizabeth B.
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
27.
A description of the active and passive sidewall-boundary-layer removal systems of the 0.3-meter transonic cryogenic tunnel
Author
Johnson, Charles B.
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
28.
Effect of Reynolds number and Mach number on flow angularity probe sensitivity
Author
Smith, Leigh Ann
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
29.
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
30.
Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel
Author
Plentovich, Elizabeth B.
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
31.
R4 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel
Author
Jenkins, Renaldo V.
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
32.
R4 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel
Author
Jenkins, Renaldo V.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, May 1986.
Online
https://purl.fdlp.gov/GPO/gpo105897
Location
Yale Internet Resource >> None
Format
Books / Online
33.
An airfoil flutter model suspension system to accomdate large static transonic airloads
Author
Reed, Wilmer H.
Published
Newport News, VA : DEI-Tech, Inc. ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
Online
http://purl.fdlp.gov/GPO/gpo21276
Location
Yale Internet Resource >> None
Format
Books / Online
34.
High Reynolds number tests of a NASA SC(3)-0712(B) airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
Author
Johnson, William G. (William Garland), 1944-
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
35.
Operating characteristics of the multiple critical venturi system and secondary calibration nozzles used for weight-flow measurements in the Langley 16-foot transonic tunnel
Author
Berrier, Bobby 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, 1985.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
36.
Performance test of laser velocimeter system for the Langley 16-Foot Transonic Tunnel
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
37.
Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
Author
Johnson, William G. (William Garland), 1944-
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
38.
Pressure distributions from high Reynolds number tests of a NASA SC(3)-0712(B) airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
Author
Johnson, William G. (William Garland), 1944-
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
39.
Static internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60 ̊
Author
Leavitt, Laurence D.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, February 1985.
Online
https://purl.fdlp.gov/GPO/gpo107941
Location
Yale Internet Resource >> None
Format
Books / Online
40.
New coherent optical techniques for National Transonic Wind Tunnel Facility
Author
Casasent, D. P. (David Paul)
Published
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, March 1984.
Online
http://purl.fdlp.gov/GPO/gpo61678
Location
Yale Internet Resource >> None
Format
Books / Online
41.
Static internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to 60°
Author
Berrier, Bobby L.
Published
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, October 1984.
Online
http://purl.fdlp.gov/GPO/gpo76455
Location
Yale Internet Resource >> None
Format
Books / Online
42.
Static internal performance of single-expansion-ramp nozzles with various combinations of internal geometric parameters
Author
Re, Richard J.
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.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
43.
Application of laser velocimetry to unsteady flows in large scale high speed tunnels
Author
Owen, F. Kevin
Published
Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, [1983?]
Online
https://purl.fdlp.gov/GPO/gpo92845
Location
Yale Internet Resource >> None
Format
Books / Online
44.
Development of a distributed-parameter mathematical model for simulation of cryogenic wind tunnels
Author
Tripp, John S.
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.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
45.
Evaluation of turbulence induced noise in coherent anti-stokes Raman scattering
Author
Elliott, Richard A.
Published
Moffett Field, California : NASA-Ames Research Center, [1982]
Online
https://purl.fdlp.gov/GPO/gpo92557
Location
Yale Internet Resource >> None
Format
Books / Online
46.
Image degradation in 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], 1982.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
47.
Sensitivity analysis of cool-down strategies for a transonic cryogenic tunnel
Author
Thibodeaux, Jerry J.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
48.
An application of multivariable design techniques to the control of the National Transonic Facility
Author
Armstrong, Ernest S.
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.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
49.
Comparison of experimental and theoretical turbulance reduction characteristics for screens, honeycomb, and honeycomb-screen combinations
Author
Scheiman, James
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.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
50.
Comparison of experimental and theoretical turbulence reduction characteristics for screens, honeycomb, and honeycomb-screen combinations
Author
Scheiman, James
Published
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1981.
Online
https://purl.fdlp.gov/GPO/gpo172566
Location
Yale Internet Resource >> None
Format
Books / Online