Heat Transfer Mechanisms — Question 4

Section 18-11 · Physics pages 3018–3019

Question 4 Cylindrical conduction depends on a logarithmic radius ratio A cylindrical insulating shell of length 2.00 m has inner radius .0200 m, outer radius .0400 m, and conductivity .200 W/(m K). Its inner and outer surfaces are held at 360 K and 300 K. Neglect end effects. At radius r, use steady P = −k(2πrL)dT/dr. ri ro length L Schematic; labels, not drawing lengths, specify the data. (a) Integrate to obtain the thermal resistance and heat rate. (b) Find the radius where temperature is 330 K. Compare it with the arithmetic midpoint radius.
Show solutionHide solution
Question 4 - Solution Cylindrical conduction depends on a logarithmic radius ratio ri ro length L (a) Method and calculation ∫To Ti dT = − P 2πkL ∫ro ri dr r . R = ln(ro/ri) 2πkL = ln 2 .8π ≈.275795 K/W. P = 60 R ≈217.553 W. (b) Interpretation and further calculation T(r) = Ti − P 2πkL ln(r/ri). Ti −T Ti −To = ln(r/ri) ln(ro/ri) = 1 2 ⇒r = √riro = .0282843 m. The arithmetic radius midpoint is .0300 m; equal temperature drops correspond to equal logarithmic radius intervals. Physical check The transfer area increases outward, so treating the shell as a plane slab with one arbitrary surface area is not exact.

Question 4

Cylindrical conduction depends on a logarithmic radius ratio

A cylindrical insulating shell of length 2.00 m has inner radius .0200 m, outer radius .0400 m, and conductivity .200 W/(m K). Its inner and outer surfaces are held at 360 K and 300 K. Neglect end effects. At radius rr, use steady P=−k(2πrL)dT/drP=-k(2\pi rL)dT/dr.

Diagram shown in the original SVG worksheet.

  1. Integrate to obtain the thermal resistance and heat rate.

  2. Find the radius where temperature is 330 K. Compare it with the arithmetic midpoint radius.

Question 4 - Solution

Cylindrical conduction depends on a logarithmic radius ratio

Diagram shown in the original SVG worksheet.

(a) Method and calculation

∫TiTodT=−P2πkL∫rirodrr.\int_{T_i}^{T_o}dT=-\frac P{2\pi kL}\int_{r_i}^{r_o}\frac{dr}{r}.R=ln⁡(ro/ri)2πkL=ln⁡2.8π≈.275795K/W.R=\frac{\ln(r_o/r_i)}{2\pi kL}=\frac{\ln2}{.8\pi}\approx.275795\,\mathrm{K/W}.P=60R≈217.553W.P=\frac{60}{R}\approx217.553\,\mathrm W.

(b) Interpretation and further calculation

T(r)=Ti−P2πkLln⁡(r/ri).T(r)=T_i-\frac{P}{2\pi kL}\ln(r/r_i).Ti−TTi−To=ln⁡(r/ri)ln⁡(ro/ri)=12⇒r=riro=.0282843m.\frac{T_i-T}{T_i-T_o}=\frac{\ln(r/r_i)}{\ln(r_o/r_i)}=\frac12\ \Rightarrow\ r=\sqrt{r_ir_o}=.0282843\,\mathrm m.The arithmetic radius midpoint is .0300 m; equal temperature drops correspond to equal logarithmic radius intervals.

Physical check

The transfer area increases outward, so treating the shell as a plane slab with one arbitrary surface area is not exact.