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- W2023442029 abstract "Annals of the New York Academy of SciencesVolume 154, Issue 2 p. 1055-1073 RECENT TRENDS IN LOW-SPEED WIND-TUNNEL DESIGN AND TECHNIQUES R. J. Templin, R. J. Templin National Aeronautical EstablishmentNational Research Council Ottawa, CanadaSearch for more papers by this author R. J. Templin, R. J. Templin National Aeronautical EstablishmentNational Research Council Ottawa, CanadaSearch for more papers by this author First published: November 1968 https://doi.org/10.1111/j.1749-6632.1968.tb15244.xCitations: 1AboutPDF ToolsRequest permissionExport citationAdd to favoritesTrack citation ShareShare Give accessShare full text accessShare full-text accessPlease review our Terms and Conditions of Use and check box below to share full-text version of article.I have read and accept the Wiley Online Library Terms and Conditions of UseShareable LinkUse the link below to share a full-text version of this article with your friends and colleagues. Learn more.Copy URL Share a linkShare onEmailFacebookTwitterLinkedInRedditWechat REFERENCES 1 GARNER, H. C. & D. E. WALSHE. 1962. Pressure distribution and surface flow on five percent and nine percent thick wings with curved tip and 60° sweepback. U.K. Ministry of Aviation. ARC R & M No. 3244. 2 JOPPA, R. G. & V. M. GANZLER. 1964. An aerodynamic feasibility study of two- test-section wind tunnels for V/STOL testing. Paper No. 1, AIAA Aerodynamic Testing Conference, Washington , D.C. 3 WILLIAMS, J. & S. F. J. BUTLER. 1964. Further developments in low-speed wind-tunnel techniques for V/STOL and high-lift testing. Paper No. 3, AIAA Aerodynamics Testing Conference, Washington, D.C. 4 HEYSON, H. H. 1962. Linearized theory of wind-tunnel jet-boundary corrections and ground effect for VTOL-STOL aircraft. NASA TR R-124. 5 HEYSON, H. H. 1966. Wind-tunnel boundary interference for V/STOL testing. Paper No. 24, Conference on V/STOL and STOL aircraft NASA SP-116. 6 RAE, W. H. JR. 1966. An experimental investigation of the effect of test section geometry on the maximum size rotor that can be tested in a closed throat wind tunnel. AIAA Paper No. 66–736. 7 KUHN, R. E., MARK W. KELLY & CURT A. HOLZHAUSER. 1965. Bringing V/STOL's downtown. Astronautics and Aeronautics. 8 ANSCOMBE, A. & J. WILLIAMS. 1956. Some comments on high-lift testing in wind tunnels with particular reference to jet-blowing models. AGARD Report 63. 9 GRUNWALD, K. J. 1964. Wall effects and scale effects in V/STOL model testing. Paper No. 2, AIAA Aerodynamic Testing Conference, Washington, D.C. Citing Literature Volume154, Issue2International Congress on Subsonic AeronauticsNovember 1968Pages 1055-1073 ReferencesRelatedInformation" @default.
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