Thermal engineering · Heat transfer · conduction

Heat exchanger LMTD — duty, area and U

Calculate the logarithmic mean temperature difference from four terminal temperatures, apply correction factor F, then solve Q̇, A or U.

Created v1.0

By Thibaut Grzelak, Mechanical Analysis Engineer

Heat transfer · conduction
01Calculation inputs
T𝒸,inT𝒸,outT𝒸,inT𝒸,outTₕ,inTₕ,outU · AQ̇ = FUAΔTₗₘ
Q̇ = F · U · A · ΔTₗₘCalculate the logarithmic mean temperature difference from four terminal temperatures, apply correction factor F, then solve Q̇, A or U.
W/(m²·K)
02

Results

ΔTₗₘ
LMTD ΔTₗₘ
—K

Logarithmic mean temperature difference calculated from the two terminal differences.

Corrected LMTD FΔTₗₘ
—K

LMTD multiplied by the explicit correction factor F.

Terminal difference ΔT₁
—K

First terminal temperature difference for the selected flow arrangement.

Terminal difference ΔT₂
—K

Second terminal temperature difference for the selected flow arrangement.

Steady operation with known terminal bulk-fluid temperatures. The hot stream cools and the cold stream warms; both terminal differences must remain strictly positive.

01Formulas and symbols

Formulas used

↔ΔT₁ = Tₕ,in − T𝒸,out ; ΔT₂ = Tₕ,out − T𝒸,inCounterflow
→→ΔT₁ = Tₕ,in − T𝒸,in ; ΔT₂ = Tₕ,out − T𝒸,outParallel flow
ΔTₗₘ(ΔT₁ − ΔT₂) / ln(ΔT₁/ΔT₂)LMTD ΔTₗₘ
FΔTₗₘF · ΔTₗₘCorrected LMTD FΔTₗₘ
Q̇F · U · A · ΔTₗₘHeat-transfer rate Q̇
AQ̇ / (F · U · ΔTₗₘ)Heat-transfer area A
UQ̇ / (F · A · ΔTₗₘ)Overall heat-transfer coefficient U
02Assumptions and limits

Scope of validity

  • Steady operation with known terminal bulk-fluid temperatures.
  • The hot stream cools and the cold stream warms; both terminal differences must remain strictly positive.
  • The overall coefficient U is treated as constant over the whole heat-transfer area.
  • Heat loss to surroundings, energy storage and property variation are not modeled.
  • Correction factor F is an explicit engineering input between 0 and 1; this calculator does not derive F from multipass geometry.
  • Phase change, ε-NTU analysis, mass flow rates, heat capacities and pressure drop are outside scope.
03Validation example

Reference numerical case

  1. Counterflow reference: Tₕ,in = 120 °C, Tₕ,out = 80 °C, T𝒸,in = 20 °C and T𝒸,out = 60 °C.
  2. ΔT₁ = 60 K and ΔT₂ = 60 K; the analytical limit gives ΔTₗₘ = 60 K.
  3. With F = 1, U = 500 W/(m²·K) and A = 10 m², Q̇ = 300 kW.
  4. Inverse modes return A = 10 m² and U = 500 W/(m²·K) for Q̇ = 300 kW.
04References

Technical references

  1. Incropera et al. — Fundamentals of Heat and Mass Transfer: logarithmic mean temperature difference method.
  2. Kern — Process Heat Transfer: LMTD heat-exchanger sizing.
  3. NIST Special Publication 811 — SI units and temperature intervals.