Hostname: page-component-78c5997874-j824f Total loading time: 0 Render date: 2024-11-05T15:20:57.603Z Has data issue: false hasContentIssue false
  • English
  • Français

The Stability of a Thin Cantilever Beam Under an Articulated Tip Load

Published online by Cambridge University Press:  04 July 2016

B. Saravanos
B. Saravanos*
Affiliation:
Department of Aeronautical Engineering, Lanchester College of Technology, Coventry
Get access Rights & Permissions [Opens in a new window]

Extract

The lateral buckling of thin deep beams when subjected to a transverse loading system inducing bending initially in the plane of maximum flexural stiffness has been analysed on the assumption that the direction of application of the loads remains unchanged during small deformations of the beam (see, for example, treatments in Refs. 1 and 2). A typical case of a beam so loaded is illustrated in Fig. 1.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 65 , Issue 612 , December 1961 , pp. 834 - 837
Copyright
Copyright © Royal Aeronautical Society 1961

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.Timoshenko, S. (1936). Theory of Elastic Stability 1st Edition, 1936. McGraw-Hill.Google Scholar
2.Temple, G. and Bickley, W. G. (1933). Rayleigh's Principle and its Applications to Engineering^ 1st Edition, 1933. Dover Publications (1956).Google Scholar
3.Tables of Bessel Functions of Fractional Order. Prepared by the National Applied Mathematics Laboratories, National Bureau of Standards, U.S.A., 2 Vols., 1947-48. Columbia University Press, New York, N.Y., U.S.A.Google Scholar