Answer:

Step-by-step explanation:
For this case we need to make some assumptions. For example the properties not change in the time. steady conditions and that we just have conduction on the cylinder creating radial conduction.
The next step would be calculate the properties for each element at 300K using th table A.4
Air

Copper
, k=400 W/mK[/tex]
Solution to problem
Now in order to solve the problem we can use conservation of energy assuming a control volume of unit length, and we have the following equation:

And we have this :

From the correlation of Churchill we can find
like this:
![\bar Nu_(D) =0.3 +(0.62 Re^(1/2)_D Pr^(1/3))/([1+(0.4/Pr)^(2/3)]^(1/4))[1+((Re_D)/(282000))^(5/8)]^(4/5)](https://img.qammunity.org/2020/formulas/engineering/college/k5v5zu2qvalskizcsqbrzqotk1lmliyk27.png)
And if we replace we got:
![\bar Nu_(D) =0.3 +(0.62 15733.17^(1/2)_D 0.707^(1/3))/([1+(0.4/0.707)^(2/3)]^(1/4))[1+((15733.17)/(282000))^(5/8)]^(4/5) =66.17](https://img.qammunity.org/2020/formulas/engineering/college/rtawtymucs6tdb3ioa6h9kfci4ru0143tz.png)
Then we can find the value for


And finally we can calculate the surface temperature with this formula:

And replacing we have:
