Air at atmospheric pressure and 200°C flows over a plate with velocity of 5 m/s. The plate is 15 mm wide and is maintained at a temperature of 120°C. Calculate the thickness of hydrodynamic and...

Air at atmospheric pressure and 200°C flows over a plate with velocity of 5 m/s. The plate is 15 mm wide and is maintained at a temperature of 120°C. Calculate the thickness of hydrodynamic and thermal boundary layers and the heat transfer coefficient at a distance of 0.5 m from the leading edge. Assume that flow is on one side of the plate.