In: Mechanical Engineering
Hot air flows with a mass flow rate of 0.05 kg/s through an insulated square duct with side of 0.15m, the hot air enters at 103 oC and after a distance of 5m, cools to 85 oC. The heat transfer coefficient between the duct outer surface and the ambient air (Tair = 0 oC) is 6 W/m2 K.
Calculate the heat transfer coefficient between hot air and duct inner wall.
Air Cp = 1.011 KJ/kg K; air k = 0.0306 W/m K, air viscosity = 211.7*10 -7 Ns/m2; air Pr = 0.698
Cross-section area A = 0.15^2 = 0.0225 m^2
Perimeter P = 4*0.15 = 0.6 m
Hydraulic dia D = 4A/P = 4*0.0225 / 0.6 = 0.15 m
Average temperature = (103 + 85) / 2 = 94 deg C = 367 K
Air density at 94 deg C is kg/m3
Average velocity V =
= 0.05 / (0.96 * 0.0225)
V = 2.31 m/s
Reynolds number
= 0.96 * 2.31 * 0.15 / (211.7*10-7)
Re = 15746
Since Re > 2300, flow is turbulent.
Nusselt number
h * 0.15 / 0.0306 = 0.023 * 157464/5 * 0.6980.3
h = 9.6 W/m2/K