Hostname: page-component-586b7cd67f-t8hqh Total loading time: 0 Render date: 2024-11-30T17:52:37.529Z Has data issue: false hasContentIssue false
  • English
  • Français

Monoplane or Biplane?

Published online by Cambridge University Press:  28 July 2016

W. S. Farren
Get access Rights & Permissions [Opens in a new window]

Abstract

An abstract is not available for this content so a preview has been provided. Please use the Get access link above for information on how to access this content.
Image of the first page of this content. For PDF version, please use the ‘Save PDF’ preceeding this image.'
Type
Proceedings
Information
The Aeronautical Journal , Volume 33 , Issue 223 , July 1929 , pp. 489 - 540
Copyright
Copyright © Royal Aeronautical Society 1929

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

1 For details of the basis on which these have been decided, see Appendix I. and II.

2 On the Junkers J.13 the covering, including longitudinal stiffening strips, weighs between 0.7 and 0.4 lbs. per sq. ft. of double surface.

3 So far as the wings are concerned. Its effect on the tail and fuselage structure remains unchanged.

4 Two cases are dealt with, one corresponding to a wing section with a large moment coefficient (—0.05) and the other to a section such as R.A.F.15 (— 0.015). In both cases the spars are taken to be at 0.15 and 0.65 chord, and the rigidity of the front and rear lift girders is taken to be the same.