A pipe #2

Classical Mechanics Level pending

What would need to be the temperature difference Δ t \Delta t between the inner and the outer surface of a copper pipe with thermal conductivity λ = 0.9 cal cm 1 s 1 grad 1 \lambda = 0.9\ \text{cal} \cdot \text{cm}^{-1} \cdot \text{s}^{-1} \cdot \text{grad}^{-1} , and with radii r 1 = 5 cm r_1 = 5\ \text{cm} and r 2 = 6 cm r_2 = 6\ \text{cm} , if through the outer surface S = 5000 cm 2 S = 5000\ \text{cm}^2 of the pipe is supposed to radially flow an amount of heat Q = 6000 cal s 1 Q^* = 6000\ \text{cal} \cdot \text{s}^{-1} per second ?

Details and assumptions:

  • Give your answer to 2 decimal places.
  • Give your answer in C ^\circ \text{C} .


The answer is 1.46.

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1 solution

André Hucek
Oct 25, 2017

First we should define the length of the pipe l l , which gives the area surface S = 2 π r 2 l S = 2 \pi r_2 l , so

l = S 2 π r 2 = 5000 π 12 = 132.6 cm \displaystyle l = \frac{S}{2 \pi r_2} = \frac{5000}{\pi \cdot 12} = 132.6\ \text{cm} .

The heat amount per second Q = Q τ ( 1 ) from q = Q l τ = λ 2 π x d t d x \displaystyle Q^* = \frac{Q}{\tau} \hspace{4cm} \color{#3D99F6}(1)\ \small \color{#3D99F6} \text{from}\ q = \frac{Q}{l \cdot \tau} = - \lambda 2 \pi x \frac{dt}{dx}

is equal to Q = q l Q^* = q \cdot l .

So according to ( 1 ) \color{#3D99F6}(1) , we get the expression q = 2 π λ t 1 t 2 lg r 2 r 1 \displaystyle q = 2 \pi \lambda \frac{t_1 - t_2}{\text{lg} \frac{r_2}{r_1}} ,

Δ t = Q 2 π λ l ( lg r 2 lg r 1 ) = 6000 2 π 0.9 132.6 ( 4.094 3.912 ) = 1.4 6 C \implies \Delta t = \frac{Q^*}{2 \pi \lambda l} (\text{lg}\ r_2 - \text{lg}\ r_1) = \frac{6000}{2 \pi \cdot 0.9 \cdot 132.6} (4.094 - 3.912) = \boxed{1.46 ^\circ \text{C}} .

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