熱抵抗:直列の層を通る定常の熱流は、直列抵抗を流れる電流と同じように振る舞います:Q̇ = ΔT/ΣR。伝導層では R = L/(kA)、対流面では R = 1/(hA)。各層の温度降下はその熱抵抗に比例します。
各層の熱抵抗
R1 = L1/(k1A) = (100/1000)/(1.4·8) = 0.008929 K/W
R2 = L2/(k2A) = (50/1000)/(0.96·8) = 0.00651 K/W
熱流量
Q̇ = (T1 − T3)/(R1 + R2) = 27/0.01544 = 1749 W
境界面温度
最初の層で温度は Q̇·R₁ だけ下がります。
Ti = T1 − Q̇·R1 = 19 − 1749·0.008929 = 3.386 °C
答え
Ti = 3.386 °C
2.熱伝導
答え: U = 0.5256 W/(m²·K)
熱抵抗:直列の層を通る定常の熱流は、直列抵抗を流れる電流と同じように振る舞います:Q̇ = ΔT/ΣR。伝導層では R = L/(kA)、対流面では R = 1/(hA)。各層の温度降下はその熱抵抗に比例します。
直列の熱抵抗
Ri = 1/(hiA) = 1/(7.7·4) = 0.03247 K/W
R1 = L1/(k1A) = (50/1000)/(0.17·4) = 0.07353 K/W
R2 = L2/(k2A) = (50/1000)/(0.035·4) = 0.3571 K/W
Ro = 1/(hoA) = 1/(20·4) = 0.0125 K/W
ΣR = 0.4756 K/W
熱通過率
U = 1/(A·ΣR) = 1/(4·0.4756) = 0.5256 W/(m²·K)
答え
U = 0.5256 W/(m²·K)
3.熱交換器 (LMTD)
答え: A = 3.024 m²
LMTD method: the temperature difference between the streams changes along the exchanger, so the rate equation uses its logarithmic mean: Q̇ = U·A·ΔTlm, with ΔTlm = (ΔT₁ − ΔT₂)/ln(ΔT₁/ΔT₂), where ΔT₁ and ΔT₂ are the differences at the two ends. Counter-flow gives a larger ΔTlm than parallel flow for the same inlet and outlet temperatures.