A device that recovers heat from high-temperature combustion products involves passing the combustion gas between parallel plates, each of which is maintained at
(a) What is the heat flux at the plate surface?
(b) If a third plate,
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Fundamentals of Heat and Mass Transfer
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- 5.7 The average Reynolds number for air passing in turbulent flow over a 2-m-long, flat plate is . Under these conditions, the average Nusselt number was found to be equal to 4150. Determine the average heat transfer coefficient for an oil having thermal properties similar to those in Appendix 2, Table 18, at at the same Reynolds number and flowing over the same plate.arrow_forward6.1 Determine the heat transfer coefficient at the stagnation point and the average value of the heat transfer coefficient for a single 5-cm-OD, 60-cm-long tube in cross-flow. The temperature of the tube surface is , the velocity of the fluid flowing perpendicular to the tube axis is 6 m/s, and the temperature of the fluid is . Consider the following fluids: (a) air, (b) hydrogen, and (c) water.arrow_forwardA manufacturing plant produces an efluent as a waste product. As part of a waste heat recovery system, they want to use this for internal heating and cooling. The effluent is flown through a system where its temperature remains at 303.15 K. A 0.06-m diameter pipe carrying hot water and 0.04-m diameter pipe carrying cold air is passed through this effluent chamber. It can be assumed that the surface temperature of these air and water pipes are same as the effluent temperature. Water comes in at 328.15 K and exits at 308.15 K. The air comes in at 268.15 K and exits at 298.15 K. The mass flow rate of water and air is respectively, 1 kg/s and 0.01 kg/s. Determine the length of the water and air pipes in the system. Convert all calculations to C.arrow_forward
- Experiments have been conducted on a metallic cylinder 12.7 mm in diameter and 94 mm long. The cylinder is heated internally by an electrical heater and is subjected to a cross flow of air in a low-speed wind tunnel. Under a specific set of operating conditions for which the upstream air velocity and temperature were maintained at V = 10 m/s and 26.2°C, respectively, the heater power dissipation was measured to be P = 46 W, while the average cylinder surface temperature was determined to be T, = 128.4°C. It is estimated that 15% of the power dissipation is lost through the cumulative effect of surface radiation and conduction through the endpieces. Thermocouple for measuring airstream temperature Pitot tube for determining velocity Wind tunnel Power leads to electrical heater Heated cylinder Insulated endpiece Thermocouple leads 1. Determine the convection heat transfer coefficient from the experimental observations. 2. Compare the experimental result with the convection coefficient…arrow_forwardAir at 25°C flows at 50 × 10-6 kg/s within 100-mm-long channels used to cool a high thermal conductivity metal mold. Assume the flow is hydrodynamically and thermally fully developed. Air, Tmi = 25°C Mold, T=50°C- Case A Case B (a) Determine the rate of heat transferred, in W, to the air for a circular channel (D = (case A). 10 mm) when the mold temperature is 50°C (b) Consider air flowing under the same conditions as in case A, except now the channel is segmented into six smaller triangular sections. The flow area of case A is equal to the total flow area of case B. Determine the rate of heat transferred, in W, to the air for the segmented channel. (c) Determine the pressure drops for cases A and B, both in Pa.arrow_forwardAir stream at 1 atm flows with a velocity of 2 m/s, in parallel over a 3 m long square flat plate, placed on ground, where there is an unheated starting length of 1 m. The air stream has a temperature of 20 °C and the heated section of the flat plate is maintained at a constant temperature of 80 °C. Determine the local heat transfer coefficient at trailing edge and average convection heat transfer coefficient for the heated section. Also calculate the heat loss by convection. Determine the average friction coefficient and wall shear stress and drag force.arrow_forward
- Air at 2 atm. and 20oC is heated as it passes through a tube of 25 mm ID with a velocity of 10m/s. The temperature of the tube wall is maintained at 100oC. Calculate heat transfer per unit length of the tube and the bulk temperature change over a 3m length of the tubearrow_forward11B.6. Transpiration cooling in a planar system. Two large flat porous horizontal plates are sepa- rated by a relatively small distance L. The upper plate at y = L is at temperature T₁, and the lower one at y = 0 is to be maintained at a lower temperature To. To reduce the amount of heat that must be removed from the lower plate, an ideal gas at To is blown upward through both plates at a steady rate. Develop an expression for the temperature distribution and the amount of heat qo that must be removed from the cold plate per unit area as a function of the fluid properties and gas flow rate. Use the abbreviation = pCpv,L/k. Answer: edy/Let 1-e k(T₁ - To) Φ L T-TL To - TL Problems 365 ; 9⁰ =arrow_forwardFor safety reasons, parts can be directly blown by air. with dimensions of 15 cmx20 cm, which are not allowed to contact printed circuit board, 20 cm long 0.2 opened inside Cold air from a rectangular hole of cmx14 cm will be cooled. from electronic parts The heat generated is transmitted from the thin layer of the card to the duct, where it is combined with the air entering the duct at a temperature of 15 °C. is removed. The heat flux on the upper surface of the channel can be considered uniform and The heat transfer from the surfaces can be neglected. If the velocity of the air in the duct does not exceed (590) m/min and the surface temperature of the duct is constant at 50 °C, this circuit board can be safely placed on it. Calculate the maximum total power of the electronic parts to be placed.arrow_forward
- What is the length of tubing required to cool air from 80°C to 20°C via an isothermal tube maintained at 0°C? The tube diameter is 20 cm. Mean velocity of air is 4 m/s. Assume the flow to be fully-developed.arrow_forwardI need the answer as soon as possiblearrow_forwardAtmospheric air at 275 K and free stream velocity of 20 m/s flows over a 1.5 m long flat plate maintained at a uniform temperature of 325 K, calculate: (a) The average heat transfer coefficient over the region of laminar boundary layer ; (b) The average heat transfer coefficient over the entire length of 1.5 m ; (c) The total heat transfer rate from the plate to the air over 1.5 m length and 1 m wide. Assume transition occurs at Recr 2 x 105. (SNB)arrow_forward
- Principles of Heat Transfer (Activate Learning wi...Mechanical EngineeringISBN:9781305387102Author:Kreith, Frank; Manglik, Raj M.Publisher:Cengage Learning