Rectangular Fin — Temperature Distribution and Heat Transfer
Rectangular Fin — Temperature Distribution and Heat Transfer
The fin equation is a second-order ODE. Its solution depends on the tip boundary condition. The most common case assumes an insulated (adiabatic) tip, which is surprisingly accurate because the tip area is small.
$$\frac{d^2\theta}{dx^2} - m^2\theta = 0$$
where $\theta(x) = T(x) - T_\infty$ and $m = \sqrt{hP/(kA_c)}$.
$$\frac{\theta(x)}{\theta_b} = \frac{\cosh[m(L-x)]}{\cosh(mL)}$$
$$\dot{Q}_{\text{fin}} = \sqrt{hPkA_c}\,\theta_b\,\tanh(mL)$$
$\theta_b = T_b - T_\infty$.
Convection at tip: $\dot{Q} = \sqrt{hPkA_c}\,\theta_b\,\frac{\sinh(mL) + (h/mk)\cosh(mL)}{\cosh(mL) + (h/mk)\sinh(mL)}$
Corrected length (simpler): Use $L_c = L + t/2$ in the insulated-tip formula to approximate convection from the tip. Works well for thin fins.
Infinite fin ($mL > 2.5$): $\dot{Q} = \sqrt{hPkA_c}\,\theta_b$ (tanh ≈ 1)
Aluminum fin: $k = 200$, $w = 8$ cm, $t = 2$ mm, $L = 5$ cm. $h = 30$, $T_b = 100$°C, $T_\infty = 25$°C. Find $\dot{Q}_{\text{fin}}$.
$A_c = 0.08 \times 0.002 = 1.6 \times 10^{-4}$ m²
$P = 2(0.08 + 0.002) = 0.164$ m
$m = \sqrt{30 \times 0.164/(200 \times 1.6 \times 10^{-4})} = \sqrt{4.92/0.032} = \sqrt{153.75} = 12.4$ m⁻¹
$mL = 12.4 \times 0.05 = 0.620$
$\tanh(0.620) = 0.551$
$\sqrt{hPkA_c} = \sqrt{30 \times 0.164 \times 200 \times 1.6 \times 10^{-4}} = \sqrt{0.1574} = 0.397$ W/K
$\dot{Q}_{\text{fin}} = 0.397 \times 75 \times 0.551 = 16.4$ W
In Example 1, find the temperature at the fin tip.
$$\frac{\theta(L)}{\theta_b} = \frac{\cosh(0)}{\cosh(0.620)} = \frac{1}{1.198} = 0.835$$
$T_{\text{tip}} = T_\infty + 0.835 \times \theta_b = 25 + 0.835 \times 75 = 87.6$°C
The tip is 12.4°C cooler than the base — quite effective since most of the 75°C $\Delta T$ is preserved.
A steel fin ($k = 50$) with $m = 20$ m⁻¹ and $L = 15$ cm. $mL = 3.0$. Can we use the infinite fin formula?
$mL = 3.0 > 2.5$, so $\tanh(3.0) = 0.9951 \approx 1$.
Yes — the infinite fin approximation is accurate to within 0.5%. The tip is essentially at $T_\infty$.
Practice Problems
Show Answer Key
1. $\dot{Q} = 0.5 \times 60 \times \tanh(1.0) = 0.5 \times 60 \times 0.762 = 22.9$ W
2. $\theta(L)/\theta_b = 1/\cosh(2) = 1/3.762 = 0.266$. Only 26.6% of base excess temperature remains.
3. $\tanh(0.5) = 0.462$, $\tanh(1) = 0.762$, $\tanh(2) = 0.964$, $\tanh(3) = 0.995$
4. $L_c = 0.04 + 0.003/2 = 0.0415$ m
5. $mL = 1.0$. Need $P$ and $h$: from $m^2 = hP/(kA_c)$, $hP = 100 \times 180 \times 2 \times 10^{-4} = 3.6$. $\sqrt{hPkA_c} = \sqrt{3.6 \times 180 \times 2 \times 10^{-4}} = \sqrt{0.1296} = 0.360$. $\dot{Q} = 0.360 \times 50 \times 0.762 = 13.7$ W
6. $mL = 0.3$. Smaller $mL$ = slower temperature decay = more uniform. $1/\cosh(0.3) = 0.956$ vs. $1/\cosh(3) = 0.0993$.