Hostname: page-component-cd9895bd7-gbm5v Total loading time: 0 Render date: 2024-12-27T06:25:09.383Z Has data issue: false hasContentIssue false
  • English
  • Français

Secondary Stresses in Airship Hull Structures

Published online by Cambridge University Press:  28 July 2016

J. F. Baker
Get access Rights & Permissions [Opens in a new window]

Extract

In Part I. of this paper the theoretical stress analysis was given for a hexagonal braced tubular structure, supported at one end and subjected at the other to a system of longitudinal forces, giving no resultant load and no resultant couple. This tube had no bracing members in the planes of the bulkheads.

Type
Research Article
Information
The Aeronautical Journal , Volume 32 , Issue 216 , December 1928 , pp. 1021 - 1041
Copyright
Copyright © Royal Aeronautical Society 1928

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.)

References

Note on Page 1021 * The Journal of the Royal Aeronautical Society, December, 1927.

Note on Page 1021 † R.M. 948. “An experimental investigation into the properties of certain framed structures having redundant bracing members.”—A. J. S. Pippard and J. F. Baker.

Phil. Mag., July, 1925. “On an experimental verification of Castigliano’s Principle of Least Work and of a theorem relating to the torsion of a tubular framework. ”—A. J. S. Pippard and J. F. Baker.

Journal R.Ae.S., May, 1926. “The experimental analysis of frameworks with special reference to the problems of airship design.”—A. J. S. Pippard.

Note on Page 1029 * K is the ratio 30/39 obtained due to the resolution of the loads in a longitudinal direction.