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) = (150/1000)/(0.96·6) = 0.02604 K/W
R2 = L2/(k2A) = (75/1000)/(0.04·6) = 0.3125 K/W
熱流量
Q̇ = (T1 − T3)/(R1 + R2) = 37/0.3385 = 109.3 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 = 25 − 109.3·0.02604 = 22.15 °C
答え
Ti = 22.15 °C
2.熱伝導
答え: Q̇ = 22.08 W
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/(10·4) = 0.025 K/W
R1 = L1/(k1A) = (100/1000)/(0.96·4) = 0.02604 K/W
R2 = L2/(k2A) = (150/1000)/(0.035·4) = 1.071 K/W
Ro = 1/(hoA) = 1/(25·4) = 0.01 K/W
ΣR = 1.132 K/W
熱損失
Q̇ = (22 − (-3))/1.132 = 22.08 W
答え
Q̇ = 22.08 W
3.熱交換器 (LMTD)
答え: U = 3719 W/(m²·K)
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.