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A wall interference assessment/correction system [microform] / Dr. C.F. Lo, principal investigator.
Text
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
An experimental study of an adaptive-wall wind tunnel [microform] / by Zeki Celik and Leonard Roberts.
Text
Stanford, CA : Joint Institute for Aeronautics and Acoustics, Stanford University, Dept. of Aeronautics and Astronautics ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1988]
1988
0 resources
Flow in out-of-plane double s-bends [microform] / by M.C. Schmidt, J.H. Whitelaw and M. Yianneskis.
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London, England : Imperial College of Science and Technology, Fluids Section, Mechanical Enginering Dept. : [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
1986
0 resources
Derivation of jack movement influence coefficients as a basis for selecting wall contours giving reduced levels of interference in flexible walled test sections [microform] / M.J. Goodyer.
Text
Hampton, VA : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1985]
1985
0 resources
Analytical studies of boundary layer generated aircraft interior noise [microform] / M.S. Howe and P.L. Shah.
Text
Boston, MA : Boston University, College of Engineering ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel [microform] / Norbert Ulbrich.
Text
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Computer simulation of a wind tunnel test section with discrete finite-length wall slots [microform] / William B. Kemp, Jr.
Text
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986.
1986
0 resources
A wall interference assessment/correction interface measurement system for the NASA-ARC 12-FT PWT [microform] : final memorandum report.
Text
[Tullahoma, Tenn. : The University of Tennessee-Calspan Center Aerospace Research (CAR) ; Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1989]
1989
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS61599Use of adaptive walls in 2D tests [microform] / J.P. Archambaud and J.P. Chevallier.
Text
Washington, D.C. : National Aeronautics and Space Administration, [1984]
1984
0 resources
Sidewall boundary-layer effects in two-dimensional airfoil testing [microform] : progress report for the period ending June 1985 / by A.V. Murthy ; principal investigator: G.L. Goglia ; prepared for the National Aeronautics and Space Administration, Langley Research Center ; submitted by the Old Dominion University Research Foundation.
Text
Norfolk, Va. : Dept. of Mechanical Engineering and Mechanics, School of Engineering, Old Dominion University, [1985]
1985
0 resources
Data reduction functions for the Langley 14- by 22-foot subsonic tunnel / Andy D. Boney.
Text
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 2014.
2014-8
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo54991No results found from Digital Research Books Beta
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