Hostname: page-component-cd9895bd7-dzt6s Total loading time: 0 Render date: 2024-12-29T12:48:12.490Z Has data issue: false hasContentIssue false
  • English
  • Français

The General Theory of Cylindrical and Conical Tubes under Torsion and Bending Loads

Single and Many Cell Tubes of Arbitrary Cross-Sectionwith Rigid Diaphragms Part V — Concluded

Published online by Cambridge University Press:  28 July 2016

J. Hadji-Argyris  and
P. C. Dunne
Get access Rights & Permissions [Opens in a new window]

Extract

In 3.2.1 it was indicated that ξ i, η i may be found from the appropriate co-factors of the secular equation and appear directly as functions of the geometric and elastic properties of the root cross-section. The method will be applied in 5.6.2 for the four-boom tube, in 5.7.3 for the n-boom tube, and in 5.8 for the trapezoidal tube with direct stress carrying top and bottom panels. This procedure is advantageous when it is desired to study the effect on ξ, η of varying particular parameters of the cross-section.

However, when in any case the h-functions have to be obtained, it is often more expedient to determine ξ, η by one of the following procedures.

Type
Research Article
Information
The Aeronautical Journal , Volume 51 , Issue 443 , November 1947 , pp. 884 - 930
Copyright
Copyright © Royal Aeronautical Society 1947

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)