Structural Analysis II Section I.12
**
Section
I.11 Effect of
End
Restraint
**

The equations derived earlier, for pure torsion of bars with non-circular cross sections, were
based on the assumption that at any point along the length the cross section
is allowed to have out-of-plane displacement or warping.
However, when an end of the bar is fixed, it is restrained from warping - as
a result normal stresses are created on the cross section, and the assumption
of pure torsion is no longer valid.
To better understand this behavior let's consider a thin-walled bar, with an
"I" cross section, fixed at one end and free at the other where a torque is
applied.
In the vicinity of the fixed end the upper and lower
flanges of the bar act as short beams, therefore, have considerable bending
stiffness, and prevent the cross
section from warping under the applied torque. Hence, the torque is carried
mainly in the form of transverse shear in these flanges. As a result
the upper and lower flanges deflect laterally in opposite directions - referred
to as differential bending. In this case, the torque can be represented by a
couple of force H acting in each flange

At the other extreme point, near the free end,
the applied torque is carried mainly in the form of
torsional shear or
pure shear as the cross section is free to warp.
This is because, near the free end, the flanges are basically long beams with
less bending stiffness, therefore, shear rigidity dominates in this case.

At some distance **x** between the two ends
of the bar, the torque can be represented as the sum of (a) the torque taken up
by pure shear and (b) the torque taken up by transverse shear.

For angle of twist due to torsion in (a), from the analysis in
section A6.6, we can write

where the length of each rectangular portion of the cross section is assumed to
be much greater than its thickness.

For angle of twist due to torsion in (b) we use the relationship between the
lateral deflection of the flanges and the angle of twist as

Now, from mechanics of materials we can relate the flange deflection to
transverse shear force H in the flange as

Combining the pevious equations we determine angle of twist

Since the two angles of twist are equal, the right hand sides of the two
equations can be set equal to determine the ratio between the portion of
the torque taken up by transverse shear and portion taken up by pure shear.

EXAMPLE
PROBLEMS

To Section
I.10
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Pure Torsion