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Plane wall with internal heat generation

Short answer

For steady 1D conduction with uniform generation and symmetric convection cooling, the temperature distribution is T(x) = T_s + (q_g/(2k))(L^2 - x^2). Surface temperature T_s = 280 °C, maximum temperature at centre T_max = 330 °C, heat removed per face q'' = 100 kW/m^2.

A large plane plate of thickness 40 mm and thermal conductivity 20 W/m K generates heat uniformly at 5 x 10^6 W/m^3 (for example, an electrical heating element). Both faces are cooled by a fluid at 80 °C with a heat transfer coefficient of 500 W/m^2 K. Derive the temperature distribution for the plate and find (a) the surface temperature, (b) the maximum temperature and its location, and (c) the heat removed per square metre from each face.

Derivation

Let the plate occupy −L≤x≤L-L \le x \le L with 2L=402L = 40 mm, so L=0.02L = 0.02 m. For steady one-dimensional conduction with generation q˙g\dot q_g:

d2Tdx2+q˙gk=0\frac{d^2T}{dx^2} + \frac{\dot q_g}{k} = 0

Integrate: T=−q˙g2kx2+C1x+C2T = -\dfrac{\dot q_g}{2k}x^2 + C_1x + C_2. By symmetry dT/dx=0dT/dx = 0 at x=0x = 0, so C1=0C_1 = 0. At the surface x=Lx = L the conduction equals convection:

−kdTdx∣L=h (Ts−T∞)  ⇒  q˙gL=h (Ts−T∞)-k\frac{dT}{dx}\Big|_{L} = h\,(T_s - T_\infty)\;\Rightarrow\;\dot q_g L = h\,(T_s-T_\infty)

so Ts=T∞+q˙gLhT_s = T_\infty + \dfrac{\dot q_g L}{h} and

T(x)=Ts+q˙g2k(L2−x2)T(x) = T_s + \frac{\dot q_g}{2k}\left(L^2 - x^2\right)

The maximum is at the centre: Tmax=Ts+q˙gL22kT_{max} = T_s + \dfrac{\dot q_g L^2}{2k}.

(a) Surface temperature

Ts=80+(5×106)(0.02)500=80+200=280 ∘CT_s = 80 + \frac{(5\times10^6)(0.02)}{500} = 80 + 200 = 280\ ^\circ\text{C}

(b) Maximum temperature

Tmax=280+(5×106)(0.02)22(20)=280+50=330 ∘CT_{max} = 280 + \frac{(5\times10^6)(0.02)^2}{2(20)} = 280 + 50 = 330\ ^\circ\text{C}

It occurs at the mid-plane x=0x = 0.

(c) Heat removed per face

By energy balance, heat generated in the half-plate equals heat leaving one face:

q′′=q˙gL=(5×106)(0.02)=1×105 W/m2=100 kW/m2q'' = \dot q_g L = (5\times10^6)(0.02) = 1\times10^5\ \text{W/m}^2 = 100\ \text{kW/m}^2

Check: h(Ts−T∞)=500×200=1×105h(T_s - T_\infty) = 500\times200 = 1\times10^5 W/m2^2.

Answer: Ts=280 ∘T_s = 280\ ^\circC; Tmax=330 ∘T_{max} = 330\ ^\circC at the centre; q′′=100 kW/m2q'' = 100\ \text{kW/m}^2 per face.

✓ Answer checked by Claude Sonnet 5.5

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