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Book Cover
Author Neubert, M., author

Title Rectangular shell plating under uniformly distributed hydrostatic pressure / by M. Neubert and A. Sommer
Published Washington, D.C. : National Advisory Commitee for Aeronautics, [1940]


Description 1 online resource (7 pages, 3 unnumbered pages) : illustrations
Series National Advisory Committee for Aeronautics technical memorandums ; ‡v 965
Technical memorandum (United States. National Advisory Committee for Aeronautics) ; no. 965.
Summary A check of the calculation methods used by Foppl and Henky for investigating the reliability of shell plating under hydrostatic pressure has proved that the formulas yield practical results within the elastic range of the material. Foppl's approximate calculation leaves one on the safe side. It further was found on the basis of the marked ductility of the shell plating under tensile stress that the strength is from 50 to 100 percent higher in the elastic range than expected by either method
Notes "December 1940."
NACA TM No. 965
Translated from Luftfahrtforschung. Vol. 17, No. 7, pp. 207-210, July 20, 1940, by the National Advisory Commitee for Aeronautics
Bibliography Includes bibliographical references (page 7)
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. MiAaHDL
Print version record
digitized 2011 HathiTrust Digital Library committed to preserve pda MiAaHDL
Subject Shells (Engineering)
Plates (Engineering)
Hydrostatic pressure.
Strains and stresses.
Hydrostatic Pressure
shell structures.
Hydrostatic pressure.
Plates (Engineering)
Shells (Engineering)
Strains and stresses.
Form Electronic book
Author Sommer, A., author
United States. National Advisory Commitee for Aeronautics
ISBN 9781680156553
OTHER TI Technical Report Archive & Image Library (TRAIL)