Skip to main content Accessibility help

We use cookies to distinguish you from other users and to provide you with a better experience on our websites. Close this message to accept cookies or find out how to manage your cookie settings.

Close cookie message
×
  1. Home
  2. Journals
  3. The Aeronautical Journal
  4. Volume 62
Journal Home
Refine listing

Refine listing

Access:
Publication date:

Actions for selected content:

Select all | Deselect all
  • View selected items
  • Export citations
  • Download PDF (zip)
  • Save to Kindle
  • Save to Dropbox
  • Save to Google Drive

Save Search

You can save your searches here and later view and run them again in "My saved searches".

Please provide a title, maximum of 40 characters.
Cancel
×

Volume 62 - September 1958

Contents

Page 8 of 13

Technical Notes

  • Approximate Deflections in Cantilevers Curved in Plan

  • P. B. Mellor, W. Johnson
  • Published online by Cambridge University Press:
    04 July 2016, pp. 64-66

  • It is not difficult to establish equations by means of Castigliano's First Theorem intended to give the deflections and rotations at any point in a cantilever curved in plan. However, when the bending modulus, EI, and the torsional modulus, GJ, are unequal in magnitude and when the plan form is not of simple shape, these equations become difficult to handle, if not unmanageable. For the case in which EI ≃ GJ (a solid circular section or annulus) it is possible to obtain simple, approximate, and explicit expressions for the deflections under a concentrated end load of W1 and end couples M0, T0 for any form of beam. These expressions are now extended in Section 1 to take account of the end loading shown in Fig. 1.

Reviews

The Library

Other

Technical Notes

Reviews

Library

The Library

Other

Reviews

The Library

Technical Notes

  • Rear-Engined Air Liners

  • A. W. J. Smith
  • Published online by Cambridge University Press:
    04 July 2016, p. 308

  • I Should like to raise a point on the projected rear-engined jet air liners now under active consideration by several major British firms and of which “artists’ impressions” have recently been published, the latest being the V.C.10.

    The rear-engine layout has so many advantages that its use seems entirely logical, but I am curious to know whether or not such a design has been investigated with a noseplane layout in preference to the conventional tailplane. I have been interested in this possible configuration for some years and put the idea forward in a short Branch lecture at Derby when it appeared that quite a few of those then present agreed in broad principle.

Reviews

The Library

Library

Technical Notes

Other

Reviews

The Library

Page 8 of 13