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Steel Designers Manual - TheBestFriend.org

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This material is copyright - all rights reserved. Reproduced under licence from The <strong>Steel</strong> Construction Institute on 12/2/2007<br />

To buy a hardcopy version of this document call 01344 872775 or go to http://shop.steelbiz.<strong>org</strong>/<br />

<strong>Steel</strong> <strong>Designers</strong>' <strong>Manual</strong> - 6th Edition (2003)<br />

Chapter 11<br />

Plane frame analysis<br />

by JOHN RIGHINIOTIS<br />

11.1 Formulae for rigid frames<br />

11.1.1 General<br />

The formulae given in this section are based on Professor Kleinlogel’s Rahmenformeln<br />

and Mehrstielige Rahmen. 1 The formulae are applicable to frames which<br />

are symmetrical about a central vertical axis, and in which each member has constant<br />

second moment of area.<br />

Formulae are given for the following types of frame:<br />

Frame I Hingeless rectangular portal frame.<br />

Frame II Two-hinged rectangular portal frame.<br />

Frame III Hingeless gable frame with vertical legs.<br />

Frame IV Two-hinged gable frame with vertical legs.<br />

The loadings are so arranged that dead, snow and wind loads may be reproduced<br />

on all the frames. For example, wind suction acting normal to the sloping rafters of<br />

a building may be divided into horizontal and vertical components, for which appropriate<br />

formulae are given, although all the signs must be reversed because the loadings<br />

shown in the tables act inwards, not outwards as in the case of suction.<br />

It should be noted that, with few exceptions, the loads between node or panel<br />

points are uniformly distributed over the whole member. It is appreciated that it is<br />

normal practice to impose loads on frames through purlins, siderails or beams. By<br />

using the coefficients in Fig. 11.1, however, allowance can be made for many other<br />

symmetrically placed loads on the cross-beams of frames I and II shown, where the<br />

difference in effect is sufficient to warrant the corrections being made. The indeterminate<br />

BMs in the whole frame are calculated as though the loads were uniformly<br />

distributed over the beam being considered, and then all are adjusted by<br />

multiplying by the appropriate coefficient in Fig. 11.1. It may be of interest to state<br />

why these adjustments are made. In any statically indeterminate structure the indeterminate<br />

moments vary directly with the value of the following quantity:<br />

area of the free BM diagram<br />

EI<br />

Where the loaded member is of constant cross section, EI may be ignored.<br />

342

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