Introduction
A bar of uniform section fixed at one end and subject to a torque at the extreme end which is applied normal
to its axis will twist to some angle which is proportional to the applied torque. This assumes that the bar is not stressed
to a level greater than its elastic limit. This page includes various formulas which allow
calculation of the angles of twist and the resulting maximums stresses. The equations are based on the following assumptions
1) The bar is straight and of uniform section
2) The material of the bar is has uniform properties.
3) The only loading is the applied torque which is applied normal to the axis of the bar.
4) The bar is stressed within its elastic limit.
Nomenclature
T = torque (Nm)
l = length of bar (m)
J = Polar moment of inertia.(Circular Sections) ( m^{4} )
J' = Polar moment of inertia.(Non circluar sections) ( m^{4} )
K = Factor replacing J for noncircular sections.( m^{4} )
r = radial distance of point from center of section (m)
r_{o} = radius of section OD (m)
τ = shear stress (N/m^{2})
G Modulus of rigidity (N/m^{2})
θ angle of twist (radians)
Formulas
Formulas for bars of circular section
Formulas for bars of non  circular section.
Bars of non circular section tend to behave nonsymmetrically when under torque and plane sections to not remain plane. Also the distribution of
stress in a section is not necessarily linear.
The general formula of torsional stiffness of bars of noncircular section are as shown below the factor J' is dependent of the
dimensions of the section and some typical values are shown below. For the circular section J' = J.
Testing the values of J' obtained using the above equations (with η = 1) with the values obtained from the table
below the following values result.
1)Channel section 430x100x64 calculated J' = 63,118 cm^{4}. Table value 63 η = 1
2) Channel section 100x50x10 calculated J' = 2,39 cm^{4}. Table value 2,53 η = 1,06
3)Tee section 305x457x127 calculated J' = 296 cm^{4}. Table value 312 η = 1,06
4)Tee section 133x102x137 calculated J' = 2.69 cm^{4}. Table value 2,97 η = 1,10
Torsion in Sections. Structrual design
Important Note : In the notes and tables below J is used throughout for the
torsion constant for circular and non circular sections. . This is the convention in
structural design
In structural design the use of sections i.e I sections, channel section, angle sections etc.
should be avoided for applications designed to withstand torsional loading. Hollow rectangular
sections are best suited for these applications. Note: Values for J and C for square and hollow rectangular sections are provided
on webpages as indexed on webpage Sections Index
In the steel Sections tables i.e BS EN 102102: 1997"Hot finished Rectangular Hollow Sections" & BS EN 102192:"Cold Formed Circular Hollow Sections" The Torsion Constant J and the Torsion modulus constant C are
listed. These are calculated as follows.
The Torsion constant (J) for Hollow Rolled Sections are calculated as follows:
For circular hollow sections.... J = 2I
For square and rectangular hollow sections ...... J = 1/3 t^{3}h + 2k A_{h}
where:
I is the second moment of area
t is the thickness of section
h is the mean perimeter = 2 [(B  t) + (D  t)]  2 R_{c} (4  p)
A_{h} is the area enclosed by mean perimeter = (B  t) (D  t) Rc^{2} (4  p)
k =2 A_{h} t / h
B is the breadth of section
D is the depth of section
R_{c} is the average of internal and external corner radii.
Torsion modulus constant C
For circular hollow sections.............C = 2.Z
Z = elastic modulus = J /r
For square and rectangular hollow sections.............C = J / ( t + k / t )
Note: Values for J and C for square and hollow rectangular sections are provided
on webpages as indexed on webpage Sections Index

Torsional /Buckling Properties for Hot rolled Sections
A few tables providing Torsional /Buckling properties for some steel
sections are indexed below.
