Hostname: page-component-78c5997874-lj6df Total loading time: 0 Render date: 2024-11-04T19:40:04.963Z Has data issue: false hasContentIssue false
  • English
  • Français

Variable Distributed Loads in the Theorem of Three Moments

Published online by Cambridge University Press:  28 July 2016

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

Extract

The Theorem of Three Moments in a simple form, referring to bending moments at any three consecutive supports A, B, C, of a continuous beam uniform in each bay, AB = a, BG = c, takes the form

w and being constant load intensities over AB and CB respectively.

On p. 159, Vol. 42 (1938), of this journal, Capt. J. Morris discussed a modification in this case (and in the more general case when the beam is in thrust) when the load intensity varies according to a parabolic law.

Type
Research Article
Information
The Aeronautical Journal , Volume 45 , Issue 366 , June 1941 , pp. 218 - 224
Copyright
Copyright © Royal Aeronautical Society 1941

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 218 * Phil. Mag., Ser. 7, XXV., p . 852 (1938).

Note on page 218 † Berry: Trans. Roy. Aero. Soc., No. 1. The tables of values of these functions are reprinted by Pippard and Pritchard, “ Aeroplane Structures.&”

Note on page 219 * The principal error terra is given in brackets, thus [ ].

Note on page 219 † Whittaker and Robinson: Calculus of Observations, p. 155.

Note on page 222 * Whittaker and Robinson, loc. cit., p. vi