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be determined as the torque resultant of these shear flows, and the torsion section
constant I t can then be found from
T t
G d φ/ d x .
I t =
10.7.2 Analysis of statically indeterminate members
The uniform torsion of the statically indeterminate beam shown in Figure 10.17a
maybeanalysedbytakingtheleft-handreactiontorque T 0 astheredundantquan-
tity. The distribution of torque T x is therefore as shown in Figure 10.17b, and
equation 10.8 becomes
GI t d φ
d x = T 0 T x a 0 ,
where the value of the second term is taken as zero when the value inside the
Macaulay brackets is negative.
Thesolutionofthisequationwhichsatisfiestheconditionthattheangleoftwist
at the left-hand support is zero is
GI t φ = T 0 x T x a .
(10.87)
The other condition which must be satisfied is that the angle of twist at the right-
hand support must be zero. Using this in equation 10.87,
0 = T 0 L T ( L a ) ,
and so
T 0 = T ( L a )
L
.
Thusthemaximumtorqueis T 0 when a islessthan L / 2,whilethemaximumangle
of twist rotation occurs at the loaded point, and is equal to
φ a = Ta ( L a )
GI t L
.
10.8 Appendix - non-uniform torsion
10.8.1 Warping deflections
Whenamembertwists,linesoriginallyparalleltotheaxisoftwistbecomehelical,
and any element δ x × δ s × t of the section wall rotates a 0 d φ/ d x about the line a 0
 
 
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