Stress in a rod clamped between two rigid walls when the temperature is increased The usual approach to calculate stress is to equate thermal expansion in the unclamped condition to the magnitude of contraction caused by strain produced due to the walls. I have some questions about this approach:


*

*Wouldn't Young's modulus of the rod change with temperature?

*Moreover, in this method, $L$ is the length in the unclamped condition. After increasing the temperature, the 'original length' of the rod should be $L(1+\alpha \Delta T)$, which should be used in the relation (i) below because the original length of the rod is taken with reference to a particular temperature.
$$\Delta L=\frac{FL}{AY}=L\alpha \Delta T \cdots (i)$$
$$ \frac{F}{A}=Y \alpha\Delta T= \text{stress} \cdots (ii)$$
Am I correct in both? This is really bothering me because I cannot find a discussion of these points in any books, but I strongly feel their validity.
 A: The first point. 
We usually neglect the fact that Young's modulus changes with temperature.
Point 2
Now you are right the original length is just as you wrote it.
 So now if we rise the temperature in the absence of any compressive force length will be L(1+@T). So in order to keep it at the previous length strain =L@T. Now so now we will put in the young modulus formula.
A: @dawood mansoor is correct, we normally neglect temperature dependence of Young's Modulus. This is reasonable as long as the temperature range is smal and maximum temperature does not affect other relevant material properties as well (softening, in particular).  
That being said, the equation for thermal stress can be derived from the equation for mechanical stress. The main difference is that thermal stress is the result of restricting thermal expansion. See the figure below. If the right side of the bar were free, heating would result in the increase in length, $dl$, shown. The existence of a restraint (the wall shown on the right side) preventing the elongation creates thermal stress in the bar. 
For mechanical stress involving uniaxial loading and deformation the stress-strain relationship is given by
$$σ=\frac{F}{A}=Eε$$
Where $σ$ is the normal stress $E$ is Young’s modulus and $ε$ is the mechanical strain in units per unit (e.g., m/m).
Linear expansion, $dl$ due to temperature increase, is given by
$$dl=αldt$$
Where $α$ is the temperature coefficient of thermal expansion in units of $\frac{m}{m^0K}$. $l$ is the original length of the bar, and $dt$ is the temperature change.
Thermal strain for unrestricted expansion is given by 
$$ε_t=\frac{dl}{l}$$
Substituting in the previous equation we have
$$ε_t=αdt$$
With the expansion restricted, thermal stress, $ε_t$ is converted to mechanical stress $ε$ of the first equation. So setting $ε= ε_t$ in the first equation we get:
$$αdT$$
$$\frac{F}{A}=EαdT$$
Hope this helps.

A: After heating it, the length is $L_0(1+\alpha \Delta T)$ and its length has been increased by $\Delta L=L_0\alpha \Delta T$.  To get it back to its original length, we have to compress it so that the second $\Delta L$ is minus the first $\Delta L$:  $$\sigma=Y\frac{(L_0\alpha \Delta T)}{L_0(1+\alpha \Delta T)}=Y\frac{\alpha \Delta T}{(1+\alpha \Delta T)}\tag{1}$$But, from the equation for an infinite geometric progression, we have $$\frac{1}{1+\alpha \Delta T}=1-(\alpha \Delta T)+(\alpha \Delta T)^2-(\alpha \Delta T)^3+...$$If we substitute that back into Eqn. 1 and recognize that, in the approximations associated with Hooke's law, we are retaining only linear terms in the strains, we obtain (for the compressional stress):  $$\sigma=Y\alpha \Delta T$$
A: The original length of the rod is L (when the temperature is not raised), when the temperature is raised by ∆T the NATURAL TENDENCY of the rod is to stay in a length of L(1+α∆T), where α is the coefficient of linear expansion.Due to the fixed walls , the rod is being kept at a length of L , although at that temperature it should be in a length of L(α∆T) , so there is a case of compression in the rod , the compression being Lα∆TListing the components of the analysis:-natural length=L(1+α∆T)Young's modulus of elasticity of rod=Y..and other components having their usual meanings$$Lα∆T=\frac{FL(1+α∆T)}{AY}\Rightarrow F=\frac{YAα∆T}{1+α∆T}$$which is the compressive force provided by the walls from which we can get the stress diving F by A.
