Elements Of Electromagnetics
7th Edition
ISBN: 9780190698614
Author: Sadiku, Matthew N. O.
Publisher: Oxford University Press
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List and describe three methods of heat transfer. Give an example of each.
(1) Method? Example?
(2) Method? Example?
(3) Method? Example?
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- An industrial company manufactures tungsten cubes that need to be sintered to a temperature of 800K after processing. Hot combustion gas at 100OK is used to heat the tungsten cubes with a side length of 0.3m. The cube is initially at a temperature of 298K. Calculate the time that is needed for the cube to reach 800K. Be sure to show that you have verified your method is valid. 0.3m T: 1000K h: 100 W/m?/Karrow_forward2000kg cast iron housing at 450 degree Celsius is quenched in 5000kg of water at 15 degree C. What is the amount of heat transferred to water, use specific heat of water to be 4.18 kJ/kg.K and specific heat of iron to be 0.42 kJ/kg.Karrow_forwardExercise 2.3:Assume that the thermal conductivity of copper is four times that of brass. Two metalrods made of copper and brass are each 20 cm long and 2.0 cm in diameter. The rods are placed end to end. The free end of the copper rod is maintained at 1000C and the free end of the brass rod is maintained at 00C. (i) What is the equilibrium temperature at the copper-brass junction? |(ii)If the thermal conductivity of copper is 390 J/m0C, at what rate, in watts, does heat flow through the rodsarrow_forward
- Stainless steel type 304 [k = 16.3 W/m-K] from heat treatment was brought to a room @ 27C. It is in cube form and has an edge of side 20cm. Initially, the temp. of the steel from the heat treatment is 500C. The total effective heat transfer coefficient is 18 W/m2-K. How long will it take for the surface of the cube to be within 28 C of the room temp.?arrow_forwardtwo parts to a questionarrow_forwardA tube-launched rocket has stabilizing fins at its rear. During launch the fins experience hot gas at Tg = 1700 oC for a time t = 0.3 seconds. It is important that the fins survive launch without surface melting, T. Given the heat transfer coefficient is h, the heat flux per unit area is q=h(Tg-Ts). What is the objective for this design? High melting point Low thermal conductivity Launching efficiency Low melting pointarrow_forward
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