Instructional Objectives:
After reading this chapter the student will be able to
1. Make suitable approximations so that an indeterminate structure is reduced to a determinate structure.
2. Analyse indeterminate trusses by approximate methods.
3. Analyse industrial frames and portals by approximate methods.
Indeterminate trusses and industrial frames are vital elements in structural engineering, offering versatile solutions for supporting various loads and providing stability in construction. Indeterminate trusses, with their complex load distribution and redundancy, demand sophisticated analysis methods. Industrial frames, comprising columns, beams, and braces, cater to the heavy loads and dynamic forces encountered in industrial settings. Understanding the principles and design considerations of these structural systems is essential for ensuring the integrity and efficiency of diverse construction projects.
Truss:
Frame:
Indeterminate Structure:
Redundant Member:
Support Reactions:
Method of Joints:
Method of Sections:
Flexibility Method:
Stiffness Method:
Portal Frame:
Consider an indeterminate truss, which has two diagonals in each panel as shown in Fig. 35.1. This truss is commonly used for lateral bracing of building frames and as top and bottom chords of bridge truss.
This truss is externally determinate and internally statically indeterminate to 3rd degree. As discussed in lesson 10, module 2, the degree of static indeterminacy of the indeterminate planar truss is evaluated by
i = (m + r) - 2j (reproduced here for convenience)
Where m, j and r respectively are number of members, joints and unknown reaction components. Since the given truss is indeterminate to 3rd degree, it is required to make three assumptions to reduce this frame into a statically determinate truss. For the above type of trusses, two types of analysis are possible.
1. If the diagonals are going to be designed in such a way that they are equally capable of carrying either tensile or compressive forces. In such a situation, it is reasonable to assume, the shear in each panel is equally divided by two diagonals. In the context of above truss, this amounts to 3 independent assumptions (one in each panel) and hence now the structure can be solved by equations of static equilibrium alone.
2. In some cases, both the diagonals are going to be designed as long and slender. In such a case, it is reasonable to assume that panel shear is resisted by only one of its diagonals, as the compressive force carried/resisted by the other diagonal member is very small or negligible. This may be justified as the compressive diagonal buckles at very small load. Again, this leads to three independent assumptions and the truss may be solved by equations of static alone.
Generalizing the above method, it is observed that one need to make n independent assumptions to solve nth order statically indeterminate structures by equations of statics alone. The above procedure is illustrated by the following examples.
Example
Evaluate approximately forces in the truss members shown in Fig. 35.2a, assuming that the diagonals are to be designed such that they are equally capable of carrying compressive and tensile forces.
Solution:
The given frame is externally determinate and internally indeterminate to order 3. Hence reactions can be evaluated by equations of statics only. Thus,
(1)
Now it is required to make three independent assumptions to evaluate all bar forces. Based on the given information, it is assumed that, panel shear is equally resisted by both the diagonals. Hence, compressive and tensile forces in diagonals of each panel are numerically equal. Now consider the equilibrium of free body diagram of the truss shown left of A-A. This is shown in Fig. 35.2b.
For the first panel, the panel shear is 23.33 kN . Now in this panel, we have
(2)
Considering the vertical equilibrium of forces, yields
(3)
2 sinθ = 23.33
(4)
Thus,
Considering the joint , L0,
(5)
(6)
Similarly,
Now consider equilibrium of truss left of section C−C (ref. Fig. 35.2d)
(7)
It is given that
2F sinθ = 3.33
Thus,
Taking moment about U1 of all the forces,
(8)
Taking moment about L1 of all the forces,
(9)
Considering the joint equilibrium of L1 (ref. Fig. 35.2e),
(10)
Consider the equilibrium of right side of the section B − B (ref. Fig. 35.2f) the forces in the 3rd panel are evaluated.
We know that,
(11)
(12)
Considering the joint equilibrium of L3 (ref. Fig. 35.2g), yields
The bar forces in all the members of the truss are shown in Fig. 35.2h. Also in the diagram, bar forces obtained by exact method are shown in brackets.
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1. What is an indeterminate truss and how does it differ from a determinate truss? |
2. What are the advantages of using indeterminate trusses in structural design? |
3. How are indeterminate trusses analyzed and solved? |
4. What are some common applications of indeterminate trusses in practice? |
5. What are industrial frames and how do they differ from trusses? |
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