Abstract
Annals of the New York Academy of SciencesVolume 154, Issue 2 p. 672-703 FLOW PROBLEMS OF SWEPT LOW-DRAG SUCTION WINGS OF PRACTICAL CONSTRUCTION AT HIGH REYNOLDS NUMBERS* W. Pfenninger, W. Pfenninger Norair Division, Northrop Corporation Hawthorne, Calif.Search for more papers by this author W. Pfenninger, W. Pfenninger Norair Division, Northrop Corporation Hawthorne, Calif.Search for more papers by this author First published: November 1968 https://doi.org/10.1111/j.1749-6632.1968.tb15222.xCitations: 3 * Most of the work reported herein was supported by the U.S. Air Force, NASA, and FAA under contract with the AFSC Aeronautical Systems Division, Wright Patterson Air Force Base, Ohio, under the administration of P. P. Antonatos, Air Force Flight Dynamics Laboratory, Research and Technology Division. The theoretical investigations on the attachment-line boundary-layer stability of swept wings and the investigations on slot-wake fluctuations were supported by Northrop Corporation. AboutPDF 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 onFacebookTwitterLinkedInRedditWechat Citing Literature Volume154, Issue2International Congress on Subsonic AeronauticsNovember 1968Pages 672-703 RelatedInformation
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