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Hot spot temperature of a plate

Short answer

For a plate of thickness t with uniform heat generation p and both faces cooled equally, the hot-spot temperature at the centre is θ_h = θ_s + pρt²/8, where ρ is thermal resistivity. The temperature distribution is parabolic, and the rise depends on t².

What is hot spot? Taking the example of a plate of thickness t, derive the expression to find the hottest spot temperature in terms of surface temperature and thickness of plate.

A hot spot is the point of highest temperature inside a body in which heat is produced, such as a core, a coil or a conductor. Heat produced inside must flow outwards to the cooling surfaces, so the interior is hotter than the surface. Insulation near the hot spot ages fastest, so the hot-spot temperature, not the average, must be kept within the limit of the insulation class.

Derivation for a plate of thickness tt

Consider a plate whose length and width are large compared with its thickness tt, cooled equally on both faces. Then heat flows only across the thickness. Assume:

  • pp = heat (loss) produced per unit volume, W/m³, uniform
  • ρ\rho = thermal resistivity of the material, °C·m/W (ρ=1/k\rho = 1/k)
  • heat flows only in the xx direction (the other dimensions are large), and both faces are at the same surface temperature θs\theta_s.

By symmetry the hottest point is at the centre plane, x=0x = 0, where no heat crosses. Consider a plane at distance xx from the centre. All heat produced between the centre and this plane must cross it. Per unit area:

Qx=p xW/m2Q_x = p\,x \quad \text{W/m}^2

By Fourier's law, the temperature gradient is

dθdx=−ρ Qx=−ρ p x\frac{d\theta}{dx} = -\rho\, Q_x = -\rho\, p\, x

Integrating from the centre (temperature θh\theta_h):

θ(x)=θh−ρ p x22\begin{aligned} \theta(x) &= \theta_h - \frac{\rho\, p\, x^2}{2} \end{aligned}

So the temperature is parabolic across the thickness. At the surface, x=t/2x = t/2, θ=θs\theta = \theta_s:

θh−θs=ρ p2(t2)2=p ρ t28\theta_h - \theta_s = \frac{\rho\, p}{2}\left(\frac{t}{2}\right)^2 = \frac{p\,\rho\, t^2}{8}
 temperature
     ^        theta_h (hot spot)
     |         _..--.._
     |      .-'        '-.
     |    .'              '.
     |   /                  \
     |  theta_s        theta_s
     +--|---------+---------|--> x
      -t/2        0        +t/2
        <------ thickness t ------>

Result

θh=θs+p ρ t28\theta_h = \theta_s + \frac{p\,\rho\,t^2}{8}

where θh\theta_h is the hottest-spot temperature (at the mid-plane) and θs\theta_s the surface temperature.

Points to note

  • The temperature profile across the plate is a parabola with its peak at the centre.
  • The hot-spot rise above the surface is proportional to t2t^2. Halving the thickness, for example by a cooling duct in the middle, reduces it to one-quarter.
  • It is also proportional to the loss density pp and to the thermal resistivity ρ\rho. Materials with poor thermal conductivity (insulation, or laminated iron across the sheets) produce large internal gradients.
  • If only one face is cooled, the hot spot is at the insulated face, and θh−θs=pρt2/2\theta_h - \theta_s = p\rho t^2/2 (the same formula with thickness 2t2t).

✓ Answer checked by Claude Sonnet 5.5

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