3 Engineering Example 2

3.1 Torsion of a mild-steel bar

Introduction

For materials such as mild-steel, the relationship between applied shear stress and shear strain (deformation) can be described as follows.

Figure 3 summarises the relationship between shear stress and shear strain; the point ( ω Y , τ Y ) is known as the yield point .

Figure 3

PICT

Now suppose that one end of a bar of circular cross section is twisted through an angle θ , then the shear strain on the surface is given by

ω S = R θ L (2)

(where R and L are the radius and length of the bar respectively), while the shear strain, at a distance r from the central core, is given by

ω = r θ L (3)

The torque transmitted by a bar is given by the integral

T = 0 R 2 π r 2 τ ( r ) d r (4)

As the shear strain is a function of distance from the central axis of the bar, it may be that the shear strain on the surface is greater than the critical shear strain ω Y . In this scenario the shear stress is given by

τ = τ Y ω Y ω ω ω Y τ Y ω > ω Y (5)

i.e. the regions near the central axis exhibit elasticity, but in those regions near the surface the elastic limit has been exceeded and the metal exhibits plasticity (see Figure 4).

Figure 4

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Problem in words

Find an expression for the torque transmitted by a bar as a function of the angle θ through which one end is turned.

Mathematical statement of problem

Using Equations (3) to (5), find a formula for T in terms of the variable θ .

Mathematical analysis

Substituting (3) into (5)

τ = τ Y ω Y r θ L r θ L ω Y τ Y r θ L > ω Y = τ Y ω Y r θ L r L ω Y θ = r e τ Y r > L ω Y θ = r e

For small values of θ , r e R so that the whole of the bar will be in the elastic region, i.e.

τ = τ Y ω Y r θ L

Now (4) becomes

T = 0 R 2 π r 2 τ Y ω Y r θ L d r = 2 π τ Y ω Y θ L 0 R r 3 d r = 2 π τ Y ω Y θ L r 4 4 0 R = π 2 τ Y ω Y θ L R 4 (6)

i.e. the torque is directly proportional to the twist, θ .

For larger θ , r e < R , so that (4) becomes

T = 0 r e 2 π r 2 τ Y ω Y r θ L d r + r e R 2 π r 2 τ Y d r = 2 π τ Y ω Y θ L 0 r e r 3 d r + 2 π τ Y r e R r 2 d r = 2 π τ Y ω Y θ L r 4 4 0 r e + 2 π τ Y r 3 3 r e R = π 2 τ Y ω Y θ L r e 4 + 2 π 3 τ Y R 3 r e 3

But r e = L ω Y θ , so

T = π 2 τ Y ω Y θ L L 4 ω Y 4 θ 4 + 2 π 3 τ Y R 3 2 π 3 τ Y L 3 ω Y 3 θ 3 = 2 π 3 τ Y R 3 + π 1 2 τ Y 2 3 τ Y L 3 ω Y 3 θ 3 = 2 π 3 τ Y R 3 π 6 τ Y L 3 ω Y 3 θ 3 (7)

Equation (6) will apply when r e R , i.e. ( L ω Y θ ) R or θ ( L ω Y R ) , so that combining (6) and (7) gives overall

T = π 2 τ Y ω Y θ L R 4 θ L ω Y R 2 π 3 τ Y R 3 π 6 τ Y L 3 ω Y 3 θ 3 θ > L ω Y R (8)

Interpretation and further comment

At the critical value of θ , i.e. when the outer edge begins to exhibit plasticity, both formulae in (8) give

T c r i t = π 2 τ Y R 3

Furthermore, the first derivatives are both

d T d θ = π 2 τ Y ω Y R 4 L

i.e. the curves join smoothly.

The second derivatives, though, are not equal (zero in one case). In the theoretical limit as θ

T = 2 π 3 τ Y R 3

so this is the total torsional torque which can be carried by the bar. (The critical torque above is three-quarters of this value.) However, clearly θ is merely a theoretical limit since the bar would, in fact, shear at a finite value of θ .