Critical combinations of shear and direct axial stress for curved rectangular panels

A solution is presented for the problem of the buckling of curved rectangular panels subjected to combinded shear and direct axial stress. Charts giving theoretical critical combinations of shear and direct axial stress are presented for panels having five different length-width ratios.

Saved in:
Bibliographic Details
Main Author: Schildcrout, Murry.
Corporate Author: United States. National Advisory Committee for Aeronautics.
Other Authors: Stein, Manuel.
Format: eBook
Language: English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1949.
Series: Technical note (United States. National Advisory Committee for Aeronautics) ; no. 1928.
Subjects:
ISBN: 9781680156164
1680156160
Physical Description: 1 online resource (29 pages) : illustrations

Cover

Table of contents