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โค๏ธโ€๐Ÿ”ฅHeat and Mass Transfer Unit 5 Review

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5.2 Log Mean Temperature Difference (LMTD) Method

5.2 Log Mean Temperature Difference (LMTD) Method

Written by the Fiveable Content Team โ€ข Last updated August 2025
Written by the Fiveable Content Team โ€ข Last updated August 2025
โค๏ธโ€๐Ÿ”ฅHeat and Mass Transfer
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LMTD Equation for Heat Exchangers

The Log Mean Temperature Difference (LMTD) method lets you calculate the heat transfer rate in a heat exchanger by finding a single, representative temperature difference between the hot and cold fluids. A simple arithmetic average of the endpoint temperature differences would overestimate performance because the temperature profile along the exchanger isn't linear. The LMTD corrects for this by accounting for the logarithmic way temperature changes along the exchanger's length.

Derivation of the LMTD Equation

The starting point is the basic heat exchanger design equation:

Q=UAฮ”TQ = U A \Delta T

where:

  • QQ = heat transfer rate (W)
  • UU = overall heat transfer coefficient (W/mยฒยทK)
  • AA = heat transfer surface area (mยฒ)
  • ฮ”T\Delta T = temperature difference between the hot and cold fluids

The problem is that ฮ”T\Delta T varies along the length of the exchanger. To handle this, you integrate the local heat transfer over the entire length. The result of that integration gives the LMTD:

LMTD=ฮ”T1โˆ’ฮ”T2lnโก(ฮ”T1/ฮ”T2)\text{LMTD} = \frac{\Delta T_1 - \Delta T_2}{\ln(\Delta T_1 / \Delta T_2)}

  • ฮ”T1\Delta T_1 = temperature difference between the hot and cold fluids at one end of the exchanger
  • ฮ”T2\Delta T_2 = temperature difference at the other end

With the LMTD in hand, the design equation becomes:

Q=UAโ‹…LMTDQ = U A \cdot \text{LMTD}

Why not just use the arithmetic mean (ฮ”T1+ฮ”T2)/2(\Delta T_1 + \Delta T_2)/2? The arithmetic mean always overestimates the true average driving force. The LMTD is smaller and more accurate because it properly weights the exponential decay of the temperature difference. The two values converge only when ฮ”T1โ‰ˆฮ”T2\Delta T_1 \approx \Delta T_2.

Quick check: If ฮ”T1=ฮ”T2\Delta T_1 = \Delta T_2, the LMTD formula gives 0/0. In that special case, LMTD simply equals ฮ”T1\Delta T_1 (apply L'Hรดpital's rule to confirm).

Assumptions and Limitations of the LMTD Equation

The LMTD derivation relies on several idealizations. Keep these in mind when deciding whether the method applies to a given problem:

  • Constant UU: The overall heat transfer coefficient doesn't change along the exchanger. In reality, UU can vary if fluid properties change significantly with temperature.
  • Constant specific heats: The CpC_p values of both fluids remain fixed. This is reasonable for moderate temperature ranges but breaks down for large swings.
  • No phase change: Both fluids remain single-phase (no boiling or condensation). Phase-change problems require separate treatment because the temperature of the changing fluid stays nearly constant.
  • Steady-state operation: Flow rates, inlet temperatures, and UU don't change with time.
  • Negligible axial conduction and heat losses: Heat travels only radially (fluid-to-fluid), not along the wall, and nothing is lost to the surroundings.

LMTD Method for Heat Transfer Analysis

Derivation of the LMTD Equation, design and Analysis of a Heat Exchanger Network โ€“ Material Science Research India

Determining Heat Transfer Rate and Outlet Temperatures

The core idea is to combine the LMTD with energy balance equations for each fluid. You have three key relationships:

Design equation:

Q=UAโ‹…LMTDQ = U A \cdot \text{LMTD}

Energy balances:

  • Hot fluid: Q=mห™hโ€‰Cp,hโ€‰(Th,inโˆ’Th,out)Q = \dot{m}_h \, C_{p,h} \, (T_{h,\text{in}} - T_{h,\text{out}})
  • Cold fluid: Q=mห™cโ€‰Cp,cโ€‰(Tc,outโˆ’Tc,in)Q = \dot{m}_c \, C_{p,c} \, (T_{c,\text{out}} - T_{c,\text{in}})

where mห™\dot{m} is the mass flow rate (kg/s) and CpC_p is the specific heat capacity (J/kgยทK).

These three equations share the same QQ, so you can solve for unknowns by combining them. Typically you know the inlet temperatures, flow rates, fluid properties, UU, and AA, and you need to find the outlet temperatures and QQ.

Applicability to Different Flow Arrangements

How you define ฮ”T1\Delta T_1 and ฮ”T2\Delta T_2 depends on the flow arrangement. Getting this wrong is one of the most common mistakes.

Parallel-flow (both fluids enter at the same end):

ฮ”T1=Th,inโˆ’Tc,in\Delta T_1 = T_{h,\text{in}} - T_{c,\text{in}}

ฮ”T2=Th,outโˆ’Tc,out\Delta T_2 = T_{h,\text{out}} - T_{c,\text{out}}

Both differences are taken at the same physical end of the exchanger.

Counter-flow (fluids enter at opposite ends):

ฮ”T1=Th,inโˆ’Tc,out\Delta T_1 = T_{h,\text{in}} - T_{c,\text{out}}

ฮ”T2=Th,outโˆ’Tc,in\Delta T_2 = T_{h,\text{out}} - T_{c,\text{in}}

Each difference pairs the hot and cold temperatures at the same physical location, but because the fluids flow in opposite directions, the hot inlet faces the cold outlet.

Counter-flow exchangers always produce a higher LMTD than parallel-flow for the same inlet/outlet temperatures. That's why counter-flow is more thermally efficient and is preferred in practice.

Correction Factors for Heat Exchangers

Derivation of the LMTD Equation, Applications of Thermodynamics: Heat Pumps and Refrigerators | Physics

Purpose and Definition of Correction Factors

The LMTD formula as derived above applies directly only to pure parallel-flow and pure counter-flow arrangements. Real heat exchangers often have more complex geometries: multi-pass shell-and-tube, cross-flow with mixed or unmixed fluids, etc. In these cases, the true mean temperature difference is lower than the counter-flow LMTD.

To handle this, you multiply the counter-flow LMTD by a correction factor FF:

ฮ”Tm=Fโ‹…LMTDcounter-flow\Delta T_m = F \cdot \text{LMTD}_{\text{counter-flow}}

so the design equation becomes:

Q=UAโ€‰Fโ€‰LMTDcounter-flowQ = U A \, F \, \text{LMTD}_{\text{counter-flow}}

The correction factor satisfies 0<Fโ‰ค10 < F \leq 1. A value of F=1F = 1 means the exchanger behaves like pure counter-flow. Values below about 0.75 typically signal that the chosen configuration is thermally inefficient and a different design should be considered.

Temperature Effectiveness and Heat Capacity Rate Ratio

The correction factor FF is read from charts (or calculated from correlations) using two dimensionless parameters:

Temperature effectiveness PP:

P=Tt,outโˆ’Tt,inTs,inโˆ’Tt,inP = \frac{T_{t,\text{out}} - T_{t,\text{in}}}{T_{s,\text{in}} - T_{t,\text{in}}}

This is the ratio of the actual temperature rise of the tube-side fluid to the maximum possible temperature difference. It ranges from 0 to 1.

Heat capacity rate ratio RR:

R=Ts,inโˆ’Ts,outTt,outโˆ’Tt,in=mห™tโ€‰Cp,tmห™sโ€‰Cp,sR = \frac{T_{s,\text{in}} - T_{s,\text{out}}}{T_{t,\text{out}} - T_{t,\text{in}}} = \frac{\dot{m}_t \, C_{p,t}}{\dot{m}_s \, C_{p,s}}

Here subscripts ss and tt refer to the shell-side and tube-side fluids. RR is the ratio of the tube-side to shell-side heat capacity rates.

Different exchanger configurations (1-shell/2-tube-pass, 2-shell/4-tube-pass, cross-flow unmixed, etc.) each have their own FF-chart or correlation. Your textbook or reference tables will specify which chart to use for a given geometry.

LMTD Method for Flow Arrangements

Solving Heat Exchanger Problems

The LMTD method applies to:

  • Parallel-flow heat exchangers
  • Counter-flow heat exchangers
  • Multi-pass shell-and-tube heat exchangers
  • Cross-flow heat exchangers (one or both fluids mixed or unmixed)

Typical given information:

  • Inlet temperatures Th,inT_{h,\text{in}} and Tc,inT_{c,\text{in}}
  • Mass flow rates mห™h\dot{m}_h and mห™c\dot{m}_c
  • Specific heat capacities Cp,hC_{p,h} and Cp,cC_{p,c}
  • Overall heat transfer coefficient UU
  • Heat transfer surface area AA

Step-by-step approach:

  1. Write energy balances for both fluids to relate QQ to the unknown outlet temperatures.

  2. Calculate ฮ”T1\Delta T_1 and ฮ”T2\Delta T_2 using the correct definitions for your flow arrangement (parallel or counter-flow).

  3. Compute the LMTD from (ฮ”T1โˆ’ฮ”T2)/lnโก(ฮ”T1/ฮ”T2)(\Delta T_1 - \Delta T_2) / \ln(\Delta T_1 / \Delta T_2).

  4. Determine the correction factor FF if the exchanger is multi-pass or cross-flow. Calculate PP and RR, then read FF from the appropriate chart.

  5. Apply the design equation: Q=UAโ€‰Fโ€‰LMTDQ = U A \, F \, \text{LMTD} (use F=1F = 1 for pure parallel or counter-flow).

  6. Solve for unknowns. If outlet temperatures aren't known upfront, you'll need to iterate: assume an outlet temperature, compute LMTD, find QQ, check against the energy balance, and repeat until values converge.

Common pitfall: The LMTD method is straightforward when all four temperatures are known (a "rating" problem). When you need to find outlet temperatures (a "design" problem), it becomes iterative because the LMTD itself depends on the unknowns. For design problems, the effectiveness-NTU method (covered separately) is often more direct.

Examples of Heat Exchanger Problems

Example 1 (Counter-flow): Oil enters a counter-flow heat exchanger at 150ยฐC and must be cooled using water entering at 20ยฐC. You're given the mass flow rates, specific heats, UU, and AA. To solve: write energy balances for both fluids, express ฮ”T1=Th,inโˆ’Tc,out\Delta T_1 = T_{h,\text{in}} - T_{c,\text{out}} and ฮ”T2=Th,outโˆ’Tc,in\Delta T_2 = T_{h,\text{out}} - T_{c,\text{in}}, compute LMTD, and use Q=UAโ‹…LMTDQ = UA \cdot \text{LMTD} together with the energy balances to find the outlet temperatures. Since two outlet temperatures are unknown, you'll iterate or solve the system simultaneously.

Example 2 (Multi-pass shell-and-tube): Water is heated by steam in a 1-shell/2-tube-pass exchanger. Steam enters the shell side at 120ยฐC; water enters the tubes at 25ยฐC. After computing the counter-flow LMTD, calculate PP and RR for the tube-side fluid, look up FF from the 1-shell/2-tube-pass correction factor chart, and apply Q=UAโ€‰Fโ€‰LMTDQ = UA \, F \, \text{LMTD} to find the heat transfer rate and water outlet temperature.