Consider a cuboidal furnace (l = 5 m, b = 4 m, h = 3 m), whose surfaces closely approximate
black surfaces. The base, top, and side surfaces of the furnace are maintained at uniform
temperatures of (1040) K, (840) K, and (540) K, respectively. Determine (a)
the net rate of radiation heat transfer between the base and the side surfaces, (b) the net rate of
radiation heat transfer between the base and the top surface, and (c) the net radiation heat
transfer from the base surface.
Steam in a heating system flows through tubes whose outer radius is r1 = (3) cm and whose
walls are maintained at a temperature of 127 °C. Circular aluminum fins (k = 180 W/m K) of
outer radius r2 = (6) cm and constant thickness t = 1 mm are attached to the tube. The space
between the fins is 3 mm. Heat is transferred to the surrounding air at 27 °C, with a combined
heat transfer coefficient of 60 W/m2 K. Determine the increase in heat transfer from the tube
per meter of its length as a result of adding fins
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- All information are given. Please need Correct answer!!!!arrow_forwardA long, thin-walled horizontal tube 10.0cm in diameter with an emissivity of 0.80 is maintained at 120.0°C by the passage of pressurized steam inside the tube. To reduce radiation heat transfer losses, a round, tubular radiation shield with an emissivity of 0.10 is installed surrounding the heated tube, with a gap of 1.00cm between the outside of the tube and the radiation shield. At steady-state operating conditions, the temperature of the radiation shield is measured to be 35.0°C. Calculate the total heat transfer rate per meter length assuming that the gap between the pipe and heat shield is now filled with air at a pressure of 1.00 atm.arrow_forwardA composite wall is comprised of two large plates separated by sheets of refractory insulation. In the installation process, the sheets of thickness L = 50 mm and thermal conductivity k = 0.05 W/mK are separated at 1-m intervals by gaps of width w = 10 mm. The hot and cold plates have temperatures and emissivities of T1 = 400 deg C, emissivity1 = 0.85 and T2 = 35 deg C, emissivity2 = 0.5, respectively. Assume that the plates and insulation are diffuse-gray surfaces. %3D Determine the heat loss by radiation through the gap per unit length of the composite wall (normal to the page). Recognizing that the gaps are located on a 1-m spacing, determine what fraction of the total heat loss through the composite wall is due to transfer by radiation through the insulation gap. Hot side Gap w = 10 mm A. 47 W/m, 9.2% T1 = 400°C B. 47 W/m, 10.2% L = 50 mm C. 37 W/m, 10.2% D. 37 W/m, 9.2% T2 = 35°C Cold side 1 m Insulation, k = 0.05 W/m-Karrow_forward
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