Rectangular shell plating under uniformly distributed hydrostatic pressure

Saved in:
Bibliographic Details
Main Authors Neubert, M. (Author), Sommer, A. (Author)
Corporate Author United States. National Advisory Commitee for Aeronautics
Format Electronic eBook
LanguageEnglish
Published Washington, D.C. : National Advisory Commitee for Aeronautics, [1940]
SeriesTechnical memorandum (United States. National Advisory Committee for Aeronautics) ; no. 965.
Subjects
Online AccessFull text
ISBN9781680156553
1680156551
Physical Description1 online resource (7 pages, 3 unnumbered pages) : illustrations

Cover

More Information
Abstract: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.
Item Description:"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)
ISBN:9781680156553
1680156551
Access:Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty
Physical Description:1 online resource (7 pages, 3 unnumbered pages) : illustrations