The strength of shell bodies-- theory and practice /

Bibliographic Details
Main Author: Ebner, H. (Author)
Corporate Authors: Knovel (Firm), United States. National Advisory Commitee for Aeronautics
Format: Government Document eBook
Language:English
Published: Washington, D.C. : National Advisory Commitee for Aeronautics, [1937]
Series:Technical memorandum (United States. National Advisory Committee for Aeronautics) ; no. 838.
Subjects:
Online Access:Connect to the full text of this electronic book
Description
Abstract:The monocoque form of airplane construction has introduced a number of new problems to the stress calculator and the designer. The problems for the stress calculator fall into two groups: the determination of the stress condition (shell statics) and the determination of the failing strength (shell strength). The present report summarizes the most important theoretical and experimental results on this subject.
Item Description:"September 1937."
NACA TM Number 838.
Translated from Luftfahrtforschung. Volume 14, Number 3, March 20, 1937, by the National Advisory Commitee for Aeronautics.
Physical Description:1 online resource (51 pages, 9 unnumbered pages) : illustrations.
Bibliography:Includes bibliographical references.
ISBN:9781680156560
168015656X