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Trusses are commonly used to support roofs. For a given truss geometry and load, how can you determine the forces in the truss members and thus be able to select their sizes? A more challenging question is, that for a given load, how can we design the trusses’ geometry to minimize cost?
Trusses are also used in a variety of structures like cranes and the frames of aircraft or this space station. How can you design a lightweight structure satisfying load, safety, cost specifications,
A simple truss is a planar truss which begins with a triangular element and can be expanded by adding two members and a joint. For these trusses, the number of members (M) and the number of joints (J) are related by the equation M = 2 J – 3.
When designing the members and joints of a truss, first it is necessary to determine the forces in each truss member. This is called the force analysis of a truss. When doing this, two assumptions are made:
A free-body diagram of Joint B
BC
AB
If a joint has only two non-collinear members and there is no external load or support reaction at that joint (e.g. A and D), then those two members are zero- force members. In this example members DE, DC, AF, and AB are zero force members.
You can easily prove these results by applying the equations of equilibrium to joints A and D. Zero-force members can be removed (as shown in the figure) when analyzing the truss.
If three members form a truss joint for which two of the members are collinear (e.g. joints C and D) and there is no external load or reaction at that joint, then the third noncollinear member is a zero-force member, e.g. AC and AD. Again, this can easily be proven. The zeroforce members can also be removed, as shown, on the left, for analyzing the truss further.
Given: Loads as shown on the truss Find: The forces in each member of the truss. Plan:
45
450 kN 45
FBD of pin D y (+)
Equilibrium at A P F 2sinθ P A P A
p.7 pin-jointed str. to p.9, & p. Ch.5 pp.241- 252 -
BREAK Given: Loads as shown on the truss and ignoring selfweight Find: Determine the force in all the truss members (do not forget to mention whether they are T or C).