Cover Image

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

Bibliographic Details
Main Author: Schildcrout, Murry
Corporate Authors: Knovel (Firm), 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:
Plates (Engineering)
Curvature.
Buckling (Mechanics)
Shear (Mechanics)
Strains and stresses.
Electronic books.
Online Access:Connect to the full text of this electronic book
Description
Abstract: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.
Because the actual critical compressive stress of rectangular panels having substantial curvature is known to be much lower than the theoretical value, a semi-empirical method of analysis of curved panels subjected to combined shear and direct axial stress is presented for use in design.
Item Description:"August 1949."
NACA TN Number 1928.
Electronic resource.
Physical Description:1 online resource (29 pages) : illustrations.
Bibliography:Includes bibliographical references.
ISBN:9781680156164
1680156160