29. Obtain the average temperature difference for the laminar flow of fluids over a heated plate (L × b), for constant heat flux boundary condition, in terms of the Re and the Pr numbers. For this purpose, use the result of Problem 28 and the lo- cal Nu, number for constant heat flux boundary condition given as: 1/2 Nuy = 0.453 Re2 Pr/3 (4 = constant ) where in this relation properties are developed at the film temperature. -1/2 -1/3 [Ans.: T, -Tf =1.47 Re7"² Pr %D

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Chapter1: Basic Modes Of Heat Transfer
Section: Chapter Questions
Problem 1.23P: Using the information in Problem 1.22, estimate the ambient air temperature that could cause...
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PROBLEM: 1VB-29 

FROM THE BOOK: ENGINEERING THERMOFLUIDS, M. MASSOUD. 

28. For flow over a flat plate, the average temperature difference (i.e., T, – Tf)
when the plate temperature is kept constant is readily calculated. This is not the
case if a constant heat flux to or from the surface is imposed. Use the averaging
scheme over the plate length as given by:
f(T, – Ts
-T, kdx
T, -Tf
6 dx
to find the average temperature difference. [Hint: Substitute for AT in the nu-
merator from the Nu number and for Nu number from Equation IVb.2.11 and in-
tegrate].
29. Obtain the average temperature difference for the laminar flow of fluids over
a heated plate (L × b), for constant heat flux boundary condition, in terms of the
Re and the Pr numbers. For this purpose, use the result of Problem 28 and the lo-
cal Nu, number for constant heat flux boundary condition given as:
1/2
.1/3
Nuy = 0.453 Re2² Pr'-
(4 = constant )
where in this relation properties are developed at the film temperature.
-1/2
[Ans.: T, -Tf = 1.47 Re7"2 Pr-/3 4, (LIk)].
Transcribed Image Text:28. For flow over a flat plate, the average temperature difference (i.e., T, – Tf) when the plate temperature is kept constant is readily calculated. This is not the case if a constant heat flux to or from the surface is imposed. Use the averaging scheme over the plate length as given by: f(T, – Ts -T, kdx T, -Tf 6 dx to find the average temperature difference. [Hint: Substitute for AT in the nu- merator from the Nu number and for Nu number from Equation IVb.2.11 and in- tegrate]. 29. Obtain the average temperature difference for the laminar flow of fluids over a heated plate (L × b), for constant heat flux boundary condition, in terms of the Re and the Pr numbers. For this purpose, use the result of Problem 28 and the lo- cal Nu, number for constant heat flux boundary condition given as: 1/2 .1/3 Nuy = 0.453 Re2² Pr'- (4 = constant ) where in this relation properties are developed at the film temperature. -1/2 [Ans.: T, -Tf = 1.47 Re7"2 Pr-/3 4, (LIk)].
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