A simplified method of elastic-stability analysis for thin cylindrical shells

A simplified method of elastic-stability anal ...
S. B. Batdorf, S. B. Batdorf
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Last edited by MARC Bot
December 19, 2022 | History

A simplified method of elastic-stability analysis for thin cylindrical shells

This paper develops a new method for determining the buckling stresses of cylindrical shells under various loading conditions. In part I, the equation for the equilibrium of cylindrical shells introduced by Donnell in NACA report no. 479 to find the critical stresses of cylinders in torsion is applied to find critical stresses for cylinders with simply supported edges under other loading conditions. In part II, a modified form of Donnell's equation for the equilibrium of thin cylindrical shells is derived which is equivalent to Donnell's equation but has certain advantages in physical interpretation and in ease of solution, particularly in the case of shells having clamped edges. --

Publish Date
Publisher
U.S. G.P.O.
Language
English
Pages
25

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Book Details


Edition Notes

Includes bibliographical references.

Published in
Washington, D.C
Series
Report / National Advisory Committee for Aeronautics -- no. 874, Report (United States. National Advisory Committee for Aeronautics) -- no. 874.

Classifications

Dewey Decimal Class
629.13236
Library of Congress
TL574.S7

The Physical Object

Pagination
1 online resource (25 pages)
Number of pages
25

Edition Identifiers

Open Library
OL44477677M
ISBN 10
1680156454
ISBN 13
9781680156454
OCLC/WorldCat
914550029

Work Identifiers

Work ID
OL32663341W

Source records

marc_columbia MARC record

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December 19, 2022 Created by MARC Bot Imported from marc_columbia MARC record