Critical stress of thin-walled cylinders in torsion /

Bibliographic Details
Main Author:	Batdorf, S. B.
Corporate Authors:	Knovel (Firm), United States. National Advisory Committee for Aeronautics
Other Authors:	Stein, Manuel, Schildcrout, Murry
Format:	Government Document eBook
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, 1947.
Series:	Technical note (United States. National Advisory Committee for Aeronautics) ; no. 1344.
Subjects:	Shells (Engineering) > Thin-walled structures. Cylinders. Strains and stresses. Torsion. Electronic books.
Online Access:	Connect to the full text of this electronic book

Description
Abstract:	A theoretical solution is given of the critical stress of thin-walled cylinders loaded in torsion. The results are presented in terms of a few simple formulas and curves which are applicable to a wide range of cylinder dimensions from very short cylinders of large radius to long cylinders of small radius. Theoretical results are found to be in somewhat better agreement with experimental results than previous theoretical work for the same range of cylinder dimensions.
Item Description:	"June 1947." NACA TN Number 1344. Electronic resource.
Physical Description:	1 online resource (21 pages, 5 unnumbered pages) : illustrations, tables.
Bibliography:	Includes bibliographical references.
ISBN:	9781680156041 1680156047