Title The strength of shell bodies-- theory and practice / H. Ebner

Published Washington, D.C. : National Advisory Commitee for Aeronautics, [1937]

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Description 1 online resource (51 pages, 9 unnumbered pages) : illustrations Series Technical memorandums ; number 838 Technical memorandum (United States. National Advisory Committee for Aeronautics) ; no. 838. Summary The monocoque form of airplane construction has introduced a number of new problems to the stress calculator and the designer. The problems for the stress calculator fall into two groups: the determination of the stress condition (shell statics) and the determination of the failing strength (shell strength). The present report summarizes the most important theoretical and experimental results on this subject Notes "September 1937." NACA TM No. 838 Translated from Luftfahrtforschung. Vol. 14, No. 3, March 20, 1937, by the National Advisory Commitee for Aeronautics Bibliography Includes bibliographical references Notes Master and use copy. Digital master created according to Benchmark for Faithful Digital Reproductions of Monographs and Serials, Version 1. Digital Library Federation, December 2002. http://purl.oclc.org/DLF/benchrepro0212 MiAaHDL Print version record digitized 2011 HathiTrust Digital Library committed to preserve pda MiAaHDL Subject Monocoque construction. Shells (Engineering) Strains and stresses. Mathematics. shell structures. stress. strain. applied mathematics. mathematics. Mathematics Monocoque construction Shells (Engineering) Strains and stresses Form Electronic book Author United States. National Advisory Commitee for Aeronautics ISBN 9781680156560 168015656X

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