Answer:
Temperature distribution is
![T(x)=(q)/(k)(L-x)+T](https://img.qammunity.org/2020/formulas/engineering/college/wtemroicr9qkc8pl343zp25p7vfdup0qeo.png)
Heat flux=q
Heat rate=q A
Step-by-step explanation:
We know that for no heat generation and at steady state
![(\partial^2 T)/(\partial x^2)=0](https://img.qammunity.org/2020/formulas/engineering/college/tb0uxxyxumg3agq4glh873tjc8z8n5vhel.png)
![(\partial T)/(\partial x)=a](https://img.qammunity.org/2020/formulas/engineering/college/ekz9fxfeoetepqja2rvwpldhe5niidycoq.png)
![T(x)=ax+b](https://img.qammunity.org/2020/formulas/engineering/college/mg14v3w5xv1gig3ovoczvly09dolkwjvpz.png)
a and are the constant.
Given that heat flux=q
We know that heat flux given as
![q=-K(dT)/(dx)](https://img.qammunity.org/2020/formulas/engineering/college/eu4rigixvrnu0nk4x6uvzpsuyd9xdcsau6.png)
From above we can say that
![a= -(q)/(K)](https://img.qammunity.org/2020/formulas/engineering/college/mfcwvao6al98byeyvgbu1q515kjadzdelz.png)
Alos given that when x= L temperature is T(L)=T
![T= -(q)/(K)L+b](https://img.qammunity.org/2020/formulas/engineering/college/m6lb44w0kj88cx4g70vf6qg0ckpuqlm86a.png)
![b=T+(q)/(K)L](https://img.qammunity.org/2020/formulas/engineering/college/lzx7yrso6x4z7uaxqz8tjxztvsb72q2i5x.png)
So temperature T(x)
![T(x)=-(q)/(K)x+T+(q)/(K)L](https://img.qammunity.org/2020/formulas/engineering/college/7w3fcfydonhfsx96plrsqgvu97l4yfrf8u.png)
![T(x)=(q)/(k)(L-x)+T](https://img.qammunity.org/2020/formulas/engineering/college/wtemroicr9qkc8pl343zp25p7vfdup0qeo.png)
So temperature distribution is
![T(x)=(q)/(k)(L-x)+T](https://img.qammunity.org/2020/formulas/engineering/college/wtemroicr9qkc8pl343zp25p7vfdup0qeo.png)
Heat flux=q
Heat rate=q A (where A is the cross sectional area of wall)