The transonic characteristics of 38 cambered rectangular wings of varying aspect ratio and thickness as determined by the transonic-bump technique Page: 1 of 174
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THE TRANSONIC CHARACTERISTICS OF 38 CAMBERED
RECTANGULAR WINGS OF VARYING ASPECT RATIO
AND THICKNESS AS DETERMINED BY THE
By Warren H. Nelson and Walter J. Krumm
Ames Aeronautical Laboratory
Moffett Field, Calif.
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NATIONAL ADVISORY COMMITTEE
TECHNICAL NOTE 3502
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Nelson, Warren H. & Krumm, Walter J. The transonic characteristics of 38 cambered rectangular wings of varying aspect ratio and thickness as determined by the transonic-bump technique, report, June 1955; (digital.library.unt.edu/ark:/67531/metadc57496/m1/1/: accessed November 17, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.