18 1 Introduction
remaining reactions as the external forces S
3
,S
4
,..., S
N
. Now solve this new equiva-
lent determinate problem. Notice that since it is determinate, we can see this phase
of the process as the use of a procedure for the solution of determinate problems,
which we denote by P
D
, and gain the advantages listed in §1.4.1. The output from
P
D
will be an expression for the displacement u
y
of the beam which will contain
the unknown forces S
3
,S
4
,..., S
N
and two arbitrary constants of integration — i.e. N
unknowns in all. Since there are N reactions, there must be N kinematic conditions
at the supports, which will provide N equations for the N unknowns.
This strategy can also be applied to other indeterminate problems, such as those
involving trusses or curved beams. We shall give examples in §3.10.5 where a new
energy-based method is used for the determinate procedure P
D
.
1.5.6 Torsion of circular bars
The elementary theory of torsion leads to the formula
T
J
=
τ
r
= G
φ
, (1.18)
where T is the applied torque, J is the polar second moment for the cross section,
τ
is the shear stress,
17
r is the radial distance from the axis of the bar and
φ
is
the twist per unit length. This theory is only applicable to solid or hollow circular
cylinders and can give very large errors if it is used for bars of non-axisymmetric
cross section. The torsion problem for more general cross sections is considerably
more challenging than the corresponding bending problem. The important case of
thin-walled sections, such as I-beams and box sections is discussed in Chapter 6.
1.6 Summary
In this chapter, we have discussed the rˆole of calculations in the engineering design
process and introduced some ideas and definitions from elementary mechanics of
materials. During the early stages of an engineering design, many competing con-
cepts may be under review and only a limited time is available to judge their feasi-
bility. The effective designer needs to posess insight into the qualitative behaviour
of elastic systems and make extensive use of simple approximate techniques that
provide estimates for the stresses and displacements with the absolute minimum of
calculation. More time consuming rigorous analytical and numerical methods are
appropriate at a later stage in the design process, when the geometry and loading are
largely defined.
This theme will recur throughout the remaining chapters of this book. Emphasis
will be placed on qualitative aspects of the behaviour revealed by the analytical meth-
ods discussed. Simple approximate techniques will be introduced wherever possible
17
Notice that the shear stress
τ
acts in the circumferential direction on the cross-sectional
plane z = constant. It would therefore be denoted by
σ
z
θ
in the double suffix notation in
cylindrical polar coordinates (r,
θ
,z).