Fully Restrained Tapered Bar:
Consider the bar shown in Figure that is circular in cross-section but tapering from a diameter d2 to d1 over the length L. The bar is fully restrained at its ends. Presently, let the temperature of the bar increased through ΔT.
![2476_Fully Restrained Tapered Bar.png](https://www.expertsmind.com/CMSImages/2476_Fully%20Restrained%20Tapered%20Bar.png)
Figure
If the bar were not restrained but free to expand it would have extended through an amount ΔL, given by
ΔL = α L ΔT
Because of the restraint, a compressive force P would have developed within the bar whose effect is to generate a contraction equivalent to ΔL. Under this force, a cross-section at a distance x from the larger end would have established a stress, σx, equal to P/Ax, where Ax is the area of that cross-section.
∴ σx = P/Ax = 4P/ π(d2 +(L-x)/L (d1-d2)2)
4P/ π(d1 -x/L (d1-d2)2)
The strain at that cross-section, εx, can be written as
εx = σx/E = 4P/Eπ ( d1 -x/L(d1 - d2 ) )2
Under this strain, a small element of the bar of length dx would have changed its length by d (ΔL) given by
d (ΔL) = εx dx = 4P dx/πE ( d1 -x/L (d1 - d2 ) )2
The total change in length ΔL can then be obtained by integrating the above expression.
![1812_Fully Restrained Tapered Bar1.png](https://www.expertsmind.com/CMSImages/1812_Fully%20Restrained%20Tapered%20Bar1.png)
where, a = d1 and b = d1 -d2/L
Now, on writing (a - bx) = t, we get dx =- dt/b.
Substituting these,
![2027_Fully Restrained Tapered Bar2.png](https://www.expertsmind.com/CMSImages/2027_Fully%20Restrained%20Tapered%20Bar2.png)
= 4P/ ?bE [1/a-bx]L0 = 4P/ ?E [1/d1-(d1-d2/L)x]L0 [L/d1-d2]
= 4PL/ ?Ed1d2
∴ 4PL/?Ed1d2 = L α ΔT
So the compressive force generated in the bar due to restraining the free expansion for an increase in temperature ΔT is
P = πE d1 d2 α ΔT/4
Hence, the thermal stress, σx, at a cross-section with an area of Ax is given as
σx = P/Ax = πE d1 d2 α ΔT/4 Ax = E d1 d2 α ΔT/(d1 - x/L(d1-d2))2
where x is measured from the end along with diameter d1 which is the larger end. The maximum stress, σmax, in the bar occurs at the smaller end along with diameter d2.
σmax = E d1 α ΔT/d2
For the cross-sections other than circular, the derivation can be preceded in a similar way.