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Transonic wind tunnels
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Aerofoils

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Online Results (13)
1.
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
2.
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
3.
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
4.
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
5.
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
6.
High Reynolds number tests of the NASA SC(2)-0012 airfoil in the Langley 0.3-meter transonic cryogenic tunnel
Author
Mineck, Raymond E.
Published
[Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1987.
Location
SML, Microform (Non-Circulating) >> NAS 1.15:89102
Format
Books / Microforms
7.
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
8.
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
9.
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
10.
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.
Location
SML, Microform (Non-Circulating) >> NAS 1.60:2565
Format
Books / Microforms
11.
Tables for correcting airfoil data obtained in the Langley 0.3-meter transonic cryogenic tunnel for sidewall boundary layer effects
Author
Jenkins, Renaldo V.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1986]
Location
SML, Microform (Non-Circulating) >> NAS 1.15:87723
Format
Books / Microforms
12.
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
13.
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
14.
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
15.
High Reynolds number tests of the cast 10-2/DOA 2 airfoil in the Langley 0.3-meter transonic cryogenic tunnel - phase II
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
Location
SML, Microform (Non-Circulating) >> NAS 1.15:86273
Format
Books / Microforms
16.
The status of analytical preparation for two-dimensional testing at high transonic speeds in the University of Southampton transonic self-streamlining wind tunnel
Author
Lewis, M. C.
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-3785
Format
Books
17.
High Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-meter transonic cryogenic tunnel
Published
[Washington, D.C.?] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1982.
Location
SML, Microform (Non-Circulating) >> NAS 1.15:81922
Format
Books / Microforms
18.
Evaluation of turbulence reduction devices for the Langley 8-foot Transonic Pressure Tunnel
Author
McKinney, Marion O.
Published
Washington, D.C. : National Aeronautics and Space Administration, 1981.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
19.
Evaluation of flow quality in two large NASA wind tunnels at transonic speeds
Author
Harvey, Bill
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.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
20.
Evaluation of flow quality in two large NASA wind tunnels at transonic speeds
Author
Harvey, Bill
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
SML, Microform (Non-Circulating) >> NAS 1.60:1737
Format
Books / Microforms
21.
Experimental investigation at transonic speeds of pressure distributions over wedge and circular-arc airfoil sections and evaluation of perforated-wall interference
Author
Knechtel, Earl D. (Earl Dennis)
Published
Washington, D.C. : National Aeronautics and Space Administration, 1959.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
22.
Experimental investigation at transonic speeds of pressure distributions over wedge and circular-arc airfoil sections and evaluation of perforated-wall interference
Author
Knechtel, Earl D. (Earl Dennis)
Published
Washington, D.C. : National Aeronautics and Space Administration, 1959.
Location
Library Shelving Facility (LSF) >> NASA TN D-15
Format
Books
23.
An experimental investigation of aerodynamic effects of airfoil thickness on transonic flutter characteristics
Author
Doggett, Robert V.
Published
Washington D.C. : National Aeronautics and Space Administration, 1959.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online