If you answer the whole question while clearly showing steps and explaining with
ID: 2962662 • Letter: I
Question
If you answer the whole question while clearly showing steps and explaining with correct units the whole time you will receive 5 stars! Thanks!
Explanation / Answer
Temperature is same in both units Kelvin and Degree celsius.
Given:
mass flow rate of gaseous stream, m = 20 kg/s
heat capacity of gas, Cp = 3.45 J/g deg C = 3.45*1000 J/kg deg C
Overall heat transfer coefficient, h = 570 W/(m^2 * K ) or h = 570 W/(m^2 * deg C )
Inlet temperature of hot stream, TH1 = 431 K = 157.8 C
Outlet temperature of hot stream, TH2 = 402 K = 128.8 C
Inlet temperature of cold water, TCW1 = 85 F = 29.4 C
Outlet temperature of cold water, TCW2 = 120 F = 48.9 C
Step1: Logarithmic mean temperature, LMTD = (deltaT1 - deltaT2)/(ln(deltaT1/deltaT2))
deltaT1 = TH1 - TCW2 = ( 157.8 C - 48.9 C ) = 108.9 C
deltaT2 = TH2 - TCW1 = ( 128.8 C - 29.4 C ) = 99.4 C
LMTD = ( 108.9 C - 99.4 C ) / ln ( 108.9 / 99.4 )
LMTD = 104.1 deg C
Step 2: Rate of heat transfer required, Q = m*Cp*(change in temperature of stream)
change in temperature of stream = 431 K - 402 K = 29 K = 29 deg C
So, Rate of heat transfer required, Q = m*Cp*(change in temperature of stream)
= (20 kg/s)*(3450 J/kg deg C)*( 29 deg C)
= 20*3450*29 ( kg/s)*(J/kg deg C)*(deg C)
= 2001000 J/s
= 2001000 W = 2.001* 10^6 W
Step 3:Design equation, Q = h*A*LMTD
2.001* 10^6 W = (570 W/(m^2 * deg C) )*A*(104.1 deg C)
A = 2.001* 10^6 W/ { (570 W/(m^2 * deg C) )*(104.1 deg C) }
= 2.001* 10^6/(570*104.1 ) m^2
A = 33.722m^2
Related Questions
drjack9650@gmail.com
Navigate
Integrity-first tutoring: explanations and feedback only — we do not complete graded work. Learn more.