Homework help:Heat transfer coefficient of flow over a flat plate

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The average heat transfer coefficient for a 2-m x 3-m flat plate subjected to air flow at 20°C and 7 m/s is calculated to be 12.7 W/m²K. The analysis utilizes Reynolds number (Re) and Nusselt number (Nu) equations for both laminar and turbulent flow conditions. The discussion highlights the importance of Reynolds Analogy in relating drag force to heat transfer, with the final calculations confirming the expected results. The discrepancies in earlier calculations were addressed by correctly applying the Prandtl number in the heat transfer equations.

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A 2-m x 3-m flat plate is suspended in a room, and is subjected to air flow parallel to its surfaces along its 3-m-long side. The free stream temperature and velocity of the air are 20oC and 7m/s. the total drag force acting on the plate is measured to be 0.86N. Determine the average heat transfer coefficient for the plate. Answer:h=12.7W/m2K
Properties of air at 300K(from my textbook
ρ=1.1763
c=1.007e03
μ=1.862e-05
v=1.5e-05
Pr=0.717
k=2.614e-02

Attempt at a solution
ReL=UL/v=7*3/1.5e-05=1.5e06 >5e05
xcr=(Recrv)/U=1.07

Nux,Laminar=0.332Pr1/3Rex1/2
Nux,Turbulent=(0.0296Re0.8Pr)/(1+2.11Rex-0.1(Pr-1))

Avg heat coeff
=(1/L){0xcrhx, Laminardx + xcr3hx, Turbulentdx}
= (1/L){0xcrNux, Laminar(k/x)dx + xcr3Nux, Turbulent(k/x)dx}
= ...
=14.39


I did approximate 1+2.11Rex-0.1(Pr-1) to be equal to 1 in my working because I didn't know how to integrate it. Is that acceptable? And I don't know how to use the drag force provided in this question. :x

I've been pondering over this question for a few days and I still can't get the answer please help check if my approach is correct. Thank you.
 
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Hint: The problem states the force on the plate. That implies they want you to approach it from a Reynold's Analogy standpoint.
 
Thanks, I'll give it a shot again.
 
LawrenceC said:
Hint: The problem states the force on the plate. That implies they want you to approach it from a Reynold's Analogy standpoint.

Okay thanks for the hint once again. I tried again using Reynold's Analogy.

qx/(ρcu(T-Tw))=τwx/(ρu2)hx/c=τwx/(u)

τwx = (hxu)/(c)

AτwxdA = 0.86

A(hxu)/(c)dA = 0.86

(u/c)∫AhxdA = 0.86

(u/c)∫AhxdA = 0.86

AhxdA = (0.86c)/u

avg h
= (1/A)∫AhxdA
= (1/A) (0.86c)/u

Is this approach correct now? I subbed in the values of A=12, c = 1.007e03 and u=7 but the answer I got is 10.3 instead of the given 12.7.
I think the difference might be attributed to the value of c.

Thanks in advance
 
I started off with the basic relationship:

St*Pr^2/3 = Cf/2

I don't see the Prndtl number anywhere in your computations.
 
LawrenceC said:
I started off with the basic relationship:

St*Pr^2/3 = Cf/2

I don't see the Prndtl number anywhere in your computations.

Oops, I misread my notes, the formula I used earlier was only for Pr=1 >.<

I did as you told me and I got the answer.(at least reasonably close to it) ^^ Thanks a lot!(Sorry if I annoyed you with a lot of stupid mistakes and questions)
Here is my working if anyone is interested.

Stx = Nux/(RexPr) = hx/cpU

StxPr2/3= Cfx/2=тwx/(pU2)

(hx/cpU)Pr2/3= тwx(pU2)

hx = (c/U)(Pr-2/3wx

AhxdA = (c/U)(Pr-2/3AтwxdA

Avg heat coeff
=(1/A)∫AhxdA
=(1/A)(c/U)(Pr-2/3AтwxdA

sub A=12, c=1.007e03, U=7, Pr=0.717, ∫AтwxdA = 0.86

Avg heat coeff=12.86
 

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