Analysis of the Ultimate Strength and Optimum Proportions of Multiweb Wing Structures Page: 1 of 35
34 p. : ill.View a full description of this report.
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C)NATIONAL ADVISORY COMMITTEE
FOR AERONAUTICS
TECHNICAL NOTE 3633
ANALYSIS OF THE ULTIMATE STRENGTH AND OPTIMUI PROPORTIONS
OF MULTIWEB WING STRUCTURES
By B. Walter Rosen
Langley Aeronautical Laboratory
Langley Field, Va.March 1956
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Rosen, B. Walter. Analysis of the Ultimate Strength and Optimum Proportions of Multiweb Wing Structures, report, March 1956; (https://digital.library.unt.edu/ark:/67531/metadc57902/m1/1/: accessed July 16, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.