Answer:

Step-by-step explanation:
Given that velocity=6 m/s
Temperature of surface=75 °C
Temperature of air=25 °C
Reynolds number =

It means that this is laminar flow.So Nusselt equation given as follows

Now properties of air at mean temperature of 75 °C and 25 °C (50 °C) is taken from standard table
K=0.028 W/m-K,Pr=0.71
And we also know that

Now by putting the values

Nu=406.24


So heat flux q= hΔT
q=227.49 x (75-25)
