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 69
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 69 - August 1965

Contents

Page 14 of 15

Front matter

  • AER volume 69 issue 652 Cover and Front matter

  • Published online by Cambridge University Press:
    04 July 2016, pp. f1-f4
    • Article
      • You have access
    • PDF
    • Export citation

Reviews

The Library

Other

Reviews

Library

Front matter

  • AER volume 69 issue 658 Cover and Front matter

  • Published online by Cambridge University Press:
    04 July 2016, pp. f1-f4
    • Article
      • You have access
    • PDF
    • Export citation

Reviews

Library

Research Article

  • Reinforced Fields of Triangular Elements with Linearly Varying Strain; Effect of Initial Strains

  • J. H. Argyris
  • Published online by Cambridge University Press:
    04 July 2016, pp. 799-801

  • This third technical note, on the background of the author's Main Lecture to the Society(1), illustrates the application of the technique given in ref. 2 on a simple example, and develops the basic ideas further, with particular reference to the effect of reinforcing flanges and initial loads, as may arise through differential thermal straining. A more ambitious example demonstrating the improvement achieved by the new triangle appears in ref. 1.

Reviews

Library

Research Article

  • Matrix Displacement Analysis of Anisotropic Shells by Triangular Elements

  • J. H. Argyris
  • Published online by Cambridge University Press:
    04 July 2016, pp. 801-805

  • Over the last five years or so both in the USA (especially by the active group at Berkeley under R. W. Clough(7) ) and the UK, there have been a number of attempts to incorporate the plane triangular element under bending and membrane action into a general matrix displacement analysis of shells. All investigators stressed the positive aspects of the triangular element, which arise from its adaptability to any geometrical form of the shell, but noted at the same time some serious shortcomings due to a partial satisfaction of the kinematic compatibility conditions at the boundary. Thus we have within the Matrix Displacement Method the rather unusual example of a type of element whose deficiency with respect to kinematic compatibility does not automatically ensure convergence to the exact result as the number of elements is increased.

Front matter

  • AER volume 69 issue 651 Cover and Front matter

  • Published online by Cambridge University Press:
    04 July 2016, pp. f1-f3
    • Article
      • You have access
    • PDF
    • Export citation

Reviews

Library

Front matter

  • AER volume 69 issue 649 Cover and Front matter

  • Published online by Cambridge University Press:
    04 July 2016, pp. f1-f4
    • Article
      • You have access
    • PDF
    • Export citation

Reviews

The Library

Library

The Library

Back matter

  • AER volume 69 issue 651 Cover and Back matter

  • Published online by Cambridge University Press:
    04 July 2016, p. b1
    • Article
      • You have access
    • PDF
    • Export citation

Reviews

Library

Other

Back matter

  • AER volume 69 issue 649 Cover and Back matter

  • Published online by Cambridge University Press:
    04 July 2016, p. b1
    • Article
      • You have access
    • PDF
    • Export citation

Page 14 of 15