n internal engine of a rocket (180°C furnace) generates heat flow of 23.2564 kW through a first layer of 3m diameter, 0.0065 m thick ceramic insulator ( k = 0.6 W/m °K thermal conductivity ) Determine the heat flow across the second layer of 0.05 m thick gypsum insulator with k = 0.16 W/ m °K. If outside temperature is 12°C

Principles of Heat Transfer (Activate Learning with these NEW titles from Engineering!)
8th Edition
ISBN:9781305387102
Author:Kreith, Frank; Manglik, Raj M.
Publisher:Kreith, Frank; Manglik, Raj M.
Chapter2: Steady Heat Conduction
Section: Chapter Questions
Problem 2.18P: Estimate the rate of heat loss per unit length from a 5-cm ID, 6-cm OD steel pipe covered with...
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An internal engine of a rocket (180°C furnace) generates heat flow of 23.2564 kW through a first layer of 3m diameter, 0.0065 m thick ceramic insulator ( k = 0.6 W/m °K thermal conductivity ) Determine the heat flow across the second layer of 0.05 m thick gypsum insulator with k = 0.16 W/ m °K. If outside temperature is 12°C
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