28 2. LET’S GET STARTED
w
B
w
3
2w
3
w
w
C
w
3
2w
3
w
w
D
w
3
2w
3
w
Figure 2.14: Statically-equivalent sets of applied loads distributed differently over a boundary or part
thereof do not alter the internal stresses and their distribution several characteristic dimensions (here,
measured in terms of the width, w) away from the applied loads. Here, a compression specimen is
subjected to equivalent loads (P ) over different portions of its ends: (a) full end, (b) half end, and (c)
point load. Approximately one specimen width into the bar, the state of stress is a uniform constant
stress corresponding to P =A.
2.6 COMBINED LOADING
Note To e Instructor
While students may recognize these idealized loading cases and their respective simple formulae,
we often observe that how to linearly superpose these stress components under conditions of even simple
combined loading still eludes students even after exposure to the finite element method. Here we consider a
simple illustration for which finite element analysis is both straightforward and useful in framing students’
hand calculations as benchmarks for simulation results.
SimCafe Tutorial 1: Combined Loading in an Idealized Signpost
e purpose of this case study is to illustrate how combined loading is handled in a
straightforward manner using the finite element method. It presents a case study wherein
students can perform parametric studies varying the degrees to which the combined load-
ings are dominated by either axial, bending, torsional, or transverse shear response. It also
showcases how internal stresses from combined loads are superposed in a linear analysis.
I