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9.2 Effectiveness-NTU Method and Exchanger Rating

Key Takeaways

  • The Effectiveness-NTU (epsilon-NTU) method solves heat exchanger rating problems (determining outlet temperatures and heat duty for a known surface area and flow rates) directly and non-iteratively, whereas the LMTD method requires iterative trial-and-error because Delta_T_lm depends on unknown outlet temperatures.

  • The theoretical maximum heat transfer rate is strictly constrained by the fluid stream possessing the minimum heat capacity rate: Q_max = C_min * (T_h,in - T_c,in), where C = m_dot * Cp and C_min = min(C_h, C_c); the C_min fluid experiences the maximum theoretical temperature change.

  • Exchanger effectiveness is defined as epsilon = Q / Q_max; for pure countercurrent flow, epsilon = (1 - exp[-NTU*(1 - C_r)]) / (1 - C_r * exp[-NTU*(1 - C_r)]) where capacity ratio C_r = C_min / C_max <= 1.0 and Number of Transfer Units NTU = U * A / C_min.

  • For phase-change heat exchangers (condensers, reboilers, evaporators), one stream undergoes an isothermal transition where Cp -> infinity, collapsing C_max -> infinity and C_r = 0; under this condition, the effectiveness relation collapses to epsilon = 1 - exp(-NTU) across all flow geometries.

  • The Number of Transfer Units (NTU = U * A / C_min) is a dimensionless measure of heat exchanger physical size; beyond NTU = 3.0, heat exchangers enter a severe regime of diminishing returns where doubling surface area achieves less than 5% incremental thermal recovery.

Last updated: September 2026

9.2 Effectiveness-NTU Method and Exchanger Rating

In chemical plant operations and on the NCEES PE Chemical Exam, engineers face two fundamentally distinct categories of heat exchanger problems: sizing (design) and rating (performance evaluation).

  • In a sizing problem, fluid flow rates and all four terminal temperatures are specified; the engineer uses the Log Mean Temperature Difference (LMTD) method to directly calculate the required heat transfer surface area (AA).
  • In a rating problem, an existing heat exchanger with a fixed surface area (AA) and known overall heat transfer coefficient (UU) receives streams at specified inlet temperatures (Th,in,Tc,inT_{h,in}, T_{c,in}) and flow rates. The outlet temperatures (Th,out,Tc,outT_{h,out}, T_{c,out}) and heat duty (QQ) are unknown.

Attempting to solve a rating problem with the LMTD method leads to tedious, circular trial-and-error: you must guess an outlet temperature, compute LMTD and FF, calculate QQ, update the outlet temperatures, and repeat until convergence. To eliminate iteration entirely, W. M. Kays and A. L. London formulated the Effectiveness-NTU (ϵ\epsilon-NTU) method, which solves rating problems analytically in a single direct sequence.


1. Fundamental Definitions of the ϵ\epsilon-NTU Method

1. Heat Capacity Rates (Ch,CcC_h, C_c)

The heat capacity rate (CC) represents the thermal energy carried by a flowing stream per degree of temperature change:

Ch=m˙hCp,h,Cc=m˙cCp,cC_h = \dot{m}_h C_{p,h}, \quad C_c = \dot{m}_c C_{p,c}

Where:

  • Ch,CcC_h, C_c = heat capacity rates of hot and cold fluids (W/K\text{W/K}, kW/K\text{kW/K}, or Btu/(hr⋅∘F)\text{Btu/(hr}\cdot^\circ\text{F)}).
  • m˙\dot{m} = mass flow rate (kg/s\text{kg/s} or lb/hr\text{lb/hr}).
  • CpC_p = specific heat capacity (J/(kg⋅K)\text{J/(kg}\cdot\text{K)} or Btu/(lb⋅∘F)\text{Btu/(lb}\cdot^\circ\text{F)}).

Identify the minimum and maximum heat capacity rates:

Cmin=min⁡(Ch,Cc)C_{min} = \min(C_h, C_c) Cmax=max⁡(Ch,Cc)C_{max} = \max(C_h, C_c)

2. Heat Capacity Ratio (CrC_r)

The dimensionless capacity ratio is bounded between 00 and 11:

Cr=CminCmax(0≤Cr≤1.0)C_r = \frac{C_{min}}{C_{max}} \quad (0 \le C_r \le 1.0)

3. Maximum Theoretical Heat Transfer Rate (QmaxQ_{max})

The maximum possible heat duty that could be transferred in an idealized, infinitely long countercurrent heat exchanger is governed strictly by the fluid with the minimum heat capacity rate (CminC_{min}):

Qmax=Cmin(Th,in−Tc,in)Q_{max} = C_{min} (T_{h,in} - T_{c,in})

Important

Why CminC_{min} Limits Heat Transfer:
The maximum temperature change any fluid can experience is the difference between fluid inlet temperatures: ΔToverall=Th,in−Tc,in\Delta T_{overall} = T_{h,in} - T_{c,in}. From energy balances, Q=ChΔTh=CcΔTcQ = C_h \Delta T_h = C_c \Delta T_c. Because energy is conserved, the fluid with the smaller heat capacity rate (CminC_{min}) experiences the larger temperature change (ΔTmax=Q/Cmin\Delta T_{max} = Q / C_{min}). If the fluid with CmaxC_{max} were to undergo the full temperature span (Th,in−Tc,in)(T_{h,in} - T_{c,in}), the required heat duty would force the temperature of the CminC_{min} fluid to exceed the inlet temperature of the opposing stream, violating the Second Law of Thermodynamics! Therefore, CminC_{min} always dictates QmaxQ_{max}.

4. Heat Exchanger Effectiveness (ϵ\epsilon)

Effectiveness (ϵ\epsilon) is the dimensionless ratio of the actual heat transfer rate (QQ) to the maximum theoretical heat transfer rate (QmaxQ_{max}):

ϵ≡QQmax=Ch(Th,in−Th,out)Cmin(Th,in−Tc,in)=Cc(Tc,out−Tc,in)Cmin(Th,in−Tc,in)\epsilon \equiv \frac{Q}{Q_{max}} = \frac{C_h (T_{h,in} - T_{h,out})}{C_{min} (T_{h,in} - T_{c,in})} = \frac{C_c (T_{c,out} - T_{c,in})}{C_{min} (T_{h,in} - T_{c,in})}
  • If Ch=CminC_h = C_{min} (hot fluid is limiting): ϵ=Th,in−Th,outTh,in−Tc,in\epsilon = \frac{T_{h,in} - T_{h,out}}{T_{h,in} - T_{c,in}}
  • If Cc=CminC_c = C_{min} (cold fluid is limiting): ϵ=Tc,out−Tc,inTh,in−Tc,in\epsilon = \frac{T_{c,out} - T_{c,in}}{T_{h,in} - T_{c,in}}

Effectiveness is bounded by 0≤ϵ<1.00 \le \epsilon < 1.0. Once ϵ\epsilon is determined from the exchanger geometry and operating conditions, actual duty is calculated immediately as Q=ϵQmaxQ = \epsilon Q_{max}.

5. Number of Transfer Units (NTU\text{NTU})

The Number of Transfer Units (NTU) is a dimensionless parameter that characterizes the physical thermal size of the heat exchanger relative to the stream's heat capacity:

NTU≡U⋅ACmin\text{NTU} \equiv \frac{U \cdot A}{C_{min}}

Where:

  • UU = overall heat transfer coefficient (W/(m2⋅K)\text{W/(m}^2\cdot\text{K)}).
  • AA = total surface area (m2\text{m}^2).
  • CminC_{min} = minimum heat capacity rate (W/K\text{W/K}).

2. Explicit Analytical Effectiveness Formulas

Effectiveness is a function of flow geometry, NTU\text{NTU}, and CrC_r:

ϵ=f(NTU,Cr,Flow Arrangement)\epsilon = f(\text{NTU}, C_r, \text{Flow Arrangement})

1. Pure Countercurrent Flow

  • For Cr<1.0C_r < 1.0: ϵ=1−exp⁡[−NTU(1−Cr)]1−Crexp⁡[−NTU(1−Cr)]\epsilon = \frac{1 - \exp\left[-\text{NTU}(1 - C_r)\right]}{1 - C_r \exp\left[-\text{NTU}(1 - C_r)\right]}
  • For Cr=1.0C_r = 1.0 (Balanced Exchanger, Ch=CcC_h = C_c): ϵ=NTU1+NTU\epsilon = \frac{\text{NTU}}{1 + \text{NTU}}
  • Inverse Formula (Sizing Area from Desired Effectiveness): NTU=11−Crln⁡[1−ϵCr1−ϵ](Cr<1.0)\text{NTU} = \frac{1}{1 - C_r} \ln\left[ \frac{1 - \epsilon C_r}{1 - \epsilon} \right] \quad (C_r < 1.0) NTU=ϵ1−ϵ(Cr=1.0)\text{NTU} = \frac{\epsilon}{1 - \epsilon} \quad (C_r = 1.0)

2. Pure Cocurrent / Parallel Flow

ϵ=1−exp⁡[−NTU(1+Cr)]1+Cr\epsilon = \frac{1 - \exp\left[-\text{NTU}(1 + C_r)\right]}{1 + C_r} NTU=−ln⁡[1−ϵ(1+Cr)]1+Cr\text{NTU} = -\frac{\ln\left[ 1 - \epsilon(1 + C_r) \right]}{1 + C_r}

Note

The Parallel Flow 50% Limit:
As surface area approaches infinity (NTU→∞\text{NTU} \to \infty), the exponential term exp⁡[−NTU(1+Cr)]→0\exp[-\text{NTU}(1+C_r)] \to 0. Consequently, the maximum possible effectiveness for parallel flow is: ϵmax,parallel=11+Cr\epsilon_{max, \text{parallel}} = \frac{1}{1 + C_r} When fluid heat capacities are balanced (Cr=1.0C_r = 1.0), ϵmax=1/(1+1)=0.50\epsilon_{max} = 1 / (1 + 1) = 0.50 (50%50\%). In parallel flow, fluid streams can never exchange more than half the maximum theoretical heat because they approach a common intermediate equilibrium temperature!

3. Shell-and-Tube Exchangers (1 Shell Pass, 2,4,6,…2, 4, 6, \dots Tube Passes)

For a TEMA 1-2 shell-and-tube exchanger:

ϵ1=2[1+Cr+1+Cr2⋅1+exp⁡(−NTU1+Cr2)1−exp⁡(−NTU1+Cr2)]−1\epsilon_1 = 2 \left[ 1 + C_r + \sqrt{1 + C_r^2} \cdot \frac{1 + \exp\left(-\text{NTU} \sqrt{1 + C_r^2}\right)}{1 - \exp\left(-\text{NTU} \sqrt{1 + C_r^2}\right)} \right]^{-1}

For nn identical shell passes in series (each shell containing an even number of tube passes):

ϵ=[1−ϵ1Cr1−ϵ1]n−1[1−ϵ1Cr1−ϵ1]n−Cr\epsilon = \frac{\left[ \frac{1 - \epsilon_1 C_r}{1 - \epsilon_1} \right]^n - 1}{\left[ \frac{1 - \epsilon_1 C_r}{1 - \epsilon_1} \right]^n - C_r}

4. Crossflow Exchangers (Air Coolers, Fin-Fan Exchangers)

  • Both Fluids Unmixed (e.g., plate-fin or finned-tube radiators): ϵ=1−exp⁡{NTU0.22Cr[exp⁡(−Cr⋅NTU0.78)−1]}\epsilon = 1 - \exp\left\{ \frac{\text{NTU}^{0.22}}{C_r} \left[ \exp\left(-C_r \cdot \text{NTU}^{0.78}\right) - 1 \right] \right\}
  • CmaxC_{max} Mixed, CminC_{min} Unmixed: ϵ=1Cr(1−exp⁡{−Cr[1−exp⁡(−NTU)]})\epsilon = \frac{1}{C_r} \left( 1 - \exp\left\{ -C_r \left[ 1 - \exp(-\text{NTU}) \right] \right\} \right)
  • CminC_{min} Mixed, CmaxC_{max} Unmixed: ϵ=1−exp⁡{−1Cr[1−exp⁡(−Cr⋅NTU)]}\epsilon = 1 - \exp\left\{ -\frac{1}{C_r} \left[ 1 - \exp(-C_r \cdot \text{NTU}) \right] \right\}

3. Phase Change Heat Exchangers (Cr=0C_r = 0)

In condensers, reboilers, evaporators, and steam heaters, one process stream undergoes an isothermal phase transition (T=constantT = \text{constant}). Thermodynamically, the effective heat capacity of a boiling or condensing fluid is infinite:

Cp=(∂H∂T)P→∞  ⟹  Cmax→∞C_p = \left( \frac{\partial H}{\partial T} \right)_P \to \infty \implies C_{max} \to \infty

Therefore, the heat capacity ratio is identically zero:

Cr=CminCmax=Cmin∞=0C_r = \frac{C_{min}}{C_{max}} = \frac{C_{min}}{\infty} = \mathbf{0}

Substituting Cr=0C_r = 0 into the effectiveness formulas for all heat exchanger configurations (counterflow, parallel flow, shell-and-tube, and crossflow) collapses the equations into a single universal relationship:

ϵ=1−exp⁡(−NTU)\epsilon = 1 - \exp(-\text{NTU}) NTU=−ln⁡(1−ϵ)\text{NTU} = -\ln(1 - \epsilon)

Tip

The Cr=0C_r = 0 Shortcut on the PE Exam:
Whenever an exam question involves steam condensation or liquid vaporization, flow arrangement is completely irrelevant! Counterflow, parallel flow, and shell-and-tube all yield the identical effectiveness: ϵ=1−e−NTU\epsilon = 1 - e^{-\text{NTU}}.

4. Summary Table of Effectiveness-NTU Relations across Flow Configurations

ConfigurationEffectiveness ϵ=f(NTU,Cr)\epsilon = f(\text{NTU}, C_r)Inverse Sizing NTU=f(ϵ,Cr)\text{NTU} = f(\epsilon, C_r)Asymptotic Limit as NTU→∞\text{NTU} \to \infty
Pure Counterflow (Cr<1C_r < 1)1−exp⁡[−NTU(1−Cr)]1−Crexp⁡[−NTU(1−Cr)]\frac{1 - \exp[-\text{NTU}(1 - C_r)]}{1 - C_r \exp[-\text{NTU}(1 - C_r)]}11−Crln⁡[1−ϵCr1−ϵ]\frac{1}{1 - C_r} \ln\left[\frac{1 - \epsilon C_r}{1 - \epsilon}\right]ϵ→1.00\epsilon \to 1.00 (100%100\% recovery)
Pure Counterflow (Cr=1C_r = 1)NTU1+NTU\frac{\text{NTU}}{1 + \text{NTU}}ϵ1−ϵ\frac{\epsilon}{1 - \epsilon}ϵ→1.00\epsilon \to 1.00
Pure Parallel Flow1−exp⁡[−NTU(1+Cr)]1+Cr\frac{1 - \exp[-\text{NTU}(1 + C_r)]}{1 + C_r}−ln⁡[1−ϵ(1+Cr)]1+Cr-\frac{\ln[1 - \epsilon(1 + C_r)]}{1 + C_r}ϵ→11+Cr≤0.50\epsilon \to \frac{1}{1 + C_r} \le 0.50 (for Cr=1C_r=1)
Phase Change (Cr=0C_r = 0)1−exp⁡(−NTU)1 - \exp(-\text{NTU})−ln⁡(1−ϵ)-\ln(1 - \epsilon)ϵ→1.00\epsilon \to 1.00 (all geometries)
1-2 Shell & Tube2[1+Cr+1+Cr21+e−NTU1+Cr21−e−NTU1+Cr2]−12 \left[ 1 + C_r + \sqrt{1+C_r^2} \frac{1 + e^{-\text{NTU}\sqrt{1+C_r^2}}}{1 - e^{-\text{NTU}\sqrt{1+C_r^2}}} \right]^{-1}−11+Cr2ln⁡[2/ϵ1−1−Cr−1+Cr22/ϵ1−1−Cr+1+Cr2]-\frac{1}{\sqrt{1+C_r^2}} \ln\left[ \frac{2/\epsilon_1 - 1 - C_r - \sqrt{1+C_r^2}}{2/\epsilon_1 - 1 - C_r + \sqrt{1+C_r^2}} \right]ϵ→21+Cr+1+Cr2<1.0\epsilon \to \frac{2}{1 + C_r + \sqrt{1+C_r^2}} < 1.0

5. Systematic Exchanger Rating Algorithm (Step-by-Step)

To rate an existing heat exchanger on the PE Chemical exam, follow this rigorous 7-step sequence:

[Step 1: Calculate C_h & C_c] ---> [Step 2: Find C_min, C_max, C_r] ---> [Step 3: Compute Q_max]
                                                                                  |
[Step 6: Compute Actual Q]    <--- [Step 5: Calculate epsilon]     <--- [Step 4: Compute NTU]
            |
            v
[Step 7: Solve Outlet Temps (T_h,out & T_c,out)]
  1. Compute heat capacity rates: Ch=m˙hCp,hC_h = \dot{m}_h C_{p,h} and Cc=m˙cCp,cC_c = \dot{m}_c C_{p,c}.
  2. Identify extremes: Determine Cmin,CmaxC_{min}, C_{max}, and compute Cr=Cmin/CmaxC_r = C_{min} / C_{max}.
  3. Calculate maximum heat duty: Qmax=Cmin(Th,in−Tc,in)Q_{max} = C_{min} (T_{h,in} - T_{c,in}).
  4. Evaluate Number of Transfer Units: NTU=UA/Cmin\text{NTU} = U A / C_{min}.
  5. Evaluate effectiveness ϵ\epsilon using the analytical relation corresponding to the exchanger flow arrangement.
  6. Determine operating heat duty: Q=ϵ⋅QmaxQ = \epsilon \cdot Q_{max}.
  7. Solve for stream outlet temperatures using straightforward energy balances: Th,out=Th,in−QChT_{h,out} = T_{h,in} - \frac{Q}{C_h} Tc,out=Tc,in+QCcT_{c,out} = T_{c,in} + \frac{Q}{C_c}

6. Comprehensive Worked Numerical Example: Rating an Industrial Effluent Heat Recovery Exchanger

Problem Statement

A chemical synthesis plant utilizes an existing countercurrent plate-and-frame heat exchanger to recover waste heat from a hot aqueous effluent stream to preheat cold boiler feedwater.

Exchanger and Stream Operating Data:

  • Exchanger surface area: A=45.0 m2A = 45.0\text{ m}^2
  • Overall heat transfer coefficient: U=1,250 W/(m2⋅K)U = 1,250\text{ W/(m}^2\cdot\text{K)}
  • Hot Effluent Stream: enters at Th,in=95.0∘CT_{h,in} = 95.0^\circ\text{C} with mass flow rate m˙h=12.0 kg/s\dot{m}_h = 12.0\text{ kg/s}, Cp,h=3.80 kJ/(kg⋅K)C_{p,h} = 3.80\text{ kJ/(kg}\cdot\text{K)}
  • Cold Boiler Feedwater: enters at Tc,in=20.0∘CT_{c,in} = 20.0^\circ\text{C} with mass flow rate m˙c=8.0 kg/s\dot{m}_c = 8.0\text{ kg/s}, Cp,c=4.19 kJ/(kg⋅K)C_{p,c} = 4.19\text{ kJ/(kg}\cdot\text{K)}

Calculate:

  1. The heat capacity rates ChC_h and CcC_c, identifying CminC_{min} and capacity ratio CrC_r.
  2. The maximum theoretical heat transfer rate (QmaxQ_{max}) in kW\text{kW}.
  3. The Number of Transfer Units (NTU\text{NTU}).
  4. The thermal effectiveness (ϵ\epsilon) of the countercurrent exchanger.
  5. The actual steady-state operating heat transfer rate (QQ) in kW\text{kW}.
  6. The outlet temperatures of both process streams (Th,outT_{h,out} and Tc,outT_{c,out}).
  7. Verify the solution by calculating ΔTlm\Delta T_{lm} and confirming that Q=UAΔTlmQ = U A \Delta T_{lm}.

Step 1: Heat Capacity Rates and CrC_r

Hot fluid capacity rate:

Ch=m˙hCp,h=(12.0 kg/s)×(3.80 kJ/(kg⋅K))=45.60 kW/K=45,600 W/KC_h = \dot{m}_h C_{p,h} = (12.0\text{ kg/s}) \times (3.80\text{ kJ/(kg}\cdot\text{K)}) = \mathbf{45.60\text{ kW/K}} = 45,600\text{ W/K}

Cold fluid capacity rate:

Cc=m˙cCp,c=(8.0 kg/s)×(4.19 kJ/(kg⋅K))=33.52 kW/K=33,520 W/KC_c = \dot{m}_c C_{p,c} = (8.0\text{ kg/s}) \times (4.19\text{ kJ/(kg}\cdot\text{K)}) = \mathbf{33.52\text{ kW/K}} = 33,520\text{ W/K}

Comparing rates:

Cmin=Cc=33.520 kW/K=33,520 W/KC_{min} = C_c = \mathbf{33.520\text{ kW/K}} = \mathbf{33,520\text{ W/K}} Cmax=Ch=45.600 kW/K=45,600 W/KC_{max} = C_h = \mathbf{45.600\text{ kW/K}} = \mathbf{45,600\text{ W/K}}

Heat capacity ratio:

Cr=CminCmax=33,520 W/K45,600 W/K=0.73509C_r = \frac{C_{min}}{C_{max}} = \frac{33,520\text{ W/K}}{45,600\text{ W/K}} = \mathbf{0.73509}

Step 2: Maximum Theoretical Heat Duty

Qmax=Cmin(Th,in−Tc,in)Q_{max} = C_{min} (T_{h,in} - T_{c,in}) Qmax=(33.520 kW/K)×(95.0∘C−20.0∘C)=33.520×75.0=2,514.0 kWQ_{max} = (33.520\text{ kW/K}) \times (95.0^\circ\text{C} - 20.0^\circ\text{C}) = 33.520 \times 75.0 = \mathbf{2,514.0\text{ kW}}

Step 3: Number of Transfer Units (NTU\text{NTU})

NTU=U⋅ACmin=(1,250 W/(m2⋅K))×(45.0 m2)33,520 W/K=56,250 W/K33,520 W/K=1.6781\text{NTU} = \frac{U \cdot A}{C_{min}} = \frac{(1,250\text{ W/(m}^2\cdot\text{K)}) \times (45.0\text{ m}^2)}{33,520\text{ W/K}} = \frac{56,250\text{ W/K}}{33,520\text{ W/K}} = \mathbf{1.6781}

Step 4: Exchanger Thermal Effectiveness (ϵ\epsilon)

For pure countercurrent flow with Cr=0.73509<1.0C_r = 0.73509 < 1.0:

ϵ=1−exp⁡[−NTU(1−Cr)]1−Crexp⁡[−NTU(1−Cr)]\epsilon = \frac{1 - \exp\left[-\text{NTU}(1 - C_r)\right]}{1 - C_r \exp\left[-\text{NTU}(1 - C_r)\right]}

Evaluate exponent argument:

NTU(1−Cr)=1.6781×(1−0.73509)=1.6781×0.26491=0.44455\text{NTU}(1 - C_r) = 1.6781 \times (1 - 0.73509) = 1.6781 \times 0.26491 = \mathbf{0.44455} exp⁡(−0.44455)=0.64111\exp(-0.44455) = \mathbf{0.64111}

Numerator:

Num=1−0.64111=0.35889\text{Num} = 1 - 0.64111 = \mathbf{0.35889}

Denominator:

Den=1−Crexp⁡(−0.44455)=1−(0.73509×0.64111)=1−0.47127=0.52873\text{Den} = 1 - C_r \exp(-0.44455) = 1 - (0.73509 \times 0.64111) = 1 - 0.47127 = \mathbf{0.52873}

Effectiveness:

ϵ=0.358890.52873=0.67878≈0.6788(67.88%)\epsilon = \frac{0.35889}{0.52873} = \mathbf{0.67878} \approx \mathbf{0.6788} \quad (67.88\%)

Step 5: Actual Operating Heat Duty (QQ)

Q=ϵ⋅Qmax=0.67878×2,514.0 kW=1,706.45 kW≈1,706.5 kWQ = \epsilon \cdot Q_{max} = 0.67878 \times 2,514.0\text{ kW} = \mathbf{1,706.45\text{ kW}} \approx \mathbf{1,706.5\text{ kW}}

Step 6: Stream Outlet Temperatures

Hot effluent exit temperature:

Th,out=Th,in−QCh=95.0∘C−1,706.45 kW45.60 kW/K=95.0−37.42=57.58∘CT_{h,out} = T_{h,in} - \frac{Q}{C_h} = 95.0^\circ\text{C} - \frac{1,706.45\text{ kW}}{45.60\text{ kW/K}} = 95.0 - 37.42 = \mathbf{57.58^\circ\text{C}}

Cold boiler feedwater exit temperature:

Tc,out=Tc,in+QCc=20.0∘C+1,706.45 kW33.52 kW/K=20.0+50.91=70.91∘CT_{c,out} = T_{c,in} + \frac{Q}{C_c} = 20.0^\circ\text{C} + \frac{1,706.45\text{ kW}}{33.52\text{ kW/K}} = 20.0 + 50.91 = \mathbf{70.91^\circ\text{C}}

Notice that Tc,out(70.91∘C)>Th,out(57.58∘C)T_{c,out} (70.91^\circ\text{C}) > T_{h,out} (57.58^\circ\text{C})—a significant temperature cross of 13.33∘C13.33^\circ\text{C}, which is fully achievable because plate-and-frame exchangers operate in pure countercurrent flow!


Step 7: LMTD Cross-Verification

Terminal temperature differences:

ΔT1=Th,in−Tc,out=95.0∘C−70.91∘C=24.09∘C\Delta T_1 = T_{h,in} - T_{c,out} = 95.0^\circ\text{C} - 70.91^\circ\text{C} = 24.09^\circ\text{C} ΔT2=Th,out−Tc,in=57.58∘C−20.0∘C=37.58∘C\Delta T_2 = T_{h,out} - T_{c,in} = 57.58^\circ\text{C} - 20.0^\circ\text{C} = 37.58^\circ\text{C} ΔTlm=37.58−24.09ln⁡(37.58/24.09)=13.49ln⁡(1.5600)=13.490.44469=30.336∘C\Delta T_{lm} = \frac{37.58 - 24.09}{\ln(37.58 / 24.09)} = \frac{13.49}{\ln(1.5600)} = \frac{13.49}{0.44469} = \mathbf{30.336^\circ\text{C}}

Recalculating heat duty via LMTD (F=1.00F = 1.00 for countercurrent):

Q=U⋅A⋅ΔTlm=(1,250 W/(m2⋅K))×(45.0 m2)×(30.336 K)Q = U \cdot A \cdot \Delta T_{lm} = (1,250\text{ W/(m}^2\cdot\text{K)}) \times (45.0\text{ m}^2) \times (30.336\text{ K}) Q=56,250×30.336=1,706,400 W=1,706.4 kWQ = 56,250 \times 30.336 = 1,706,400\text{ W} = \mathbf{1,706.4\text{ kW}}

(The calculation closes with 100.00%100.00\% precision, proving exact analytical consistency between the two methods).


7. Critical PE Exam Traps & Pitfalls

Trap 1: Calculating QmaxQ_{max} Using CmaxC_{max} Instead of CminC_{min}
A catastrophic exam error is evaluating Qmax=Cmax(Th,in−Tc,in)Q_{max} = C_{max} (T_{h,in} - T_{c,in}). Doing so violates the First Law of Thermodynamics: if you transfer that much heat, the temperature change of the CminC_{min} stream would exceed (Th,in−Tc,in)(T_{h,in} - T_{c,in}), meaning a cold stream would exit hotter than the entering hot stream could ever supply. Always use CminC_{min} to establish QmaxQ_{max}.

Trap 2: Neglecting the Cr=0C_r = 0 Simplification in Phase Change Operations
When an exam question specifies a boiler, evaporator, or condenser, do not attempt to calculate the mass flow rate times liquid heat capacity for the phase-changing stream! Because latent heat transfer occurs at constant temperature, Cmax→∞C_{max} \to \infty and Cr=0C_r = 0. The effectiveness collapses immediately to ϵ=1−exp⁡(−NTU)\epsilon = 1 - \exp(-\text{NTU}) for all configurations.

Trap 3: The Economic Law of Diminishing Returns for NTU>3.0\text{NTU} > 3.0
Heat exchanger surface area scales linearly with NTU\text{NTU} (A=NTU⋅Cmin/UA = \text{NTU} \cdot C_{min} / U), but effectiveness scales asymptotically ( 1−e−NTU\,1 - e^{-\text{NTU}}). For NTU=1.0\text{NTU} = 1.0, ϵ≈63%\epsilon \approx 63\%; for NTU=3.0\text{NTU} = 3.0, ϵ≈95%\epsilon \approx 95\%. Increasing NTU\text{NTU} from 3.03.0 to 6.06.0 doubles the capital cost of the heat exchanger but yields less than 4%4\% in additional heat recovery. On process optimization exam questions, sizing an exchanger for NTU>3.5\text{NTU} > 3.5 is rarely economically justified.

Test Your Knowledge

A surface condenser condenses saturated steam at T_sat = 100.0°C on the shell side (Cr = 0). Cooling water flows through the tube bundle at a heat capacity rate of Cc = 50.0 kW/K, entering at T_c,in = 25.0°C. The overall thermal conductance of the condenser is U*A = 75.0 kW/K. Using the Effectiveness-NTU method, what are the Number of Transfer Units (NTU), thermal effectiveness (epsilon), and cooling water exit temperature (T_c,out)?

A

NTU = 0.67, epsilon = 0.487, T_c,out = 61.5°C

B

NTU = 1.50, epsilon = 0.600, T_c,out = 70.0°C

C

NTU = 1.50, epsilon = 1.000, T_c,out = 100.0°C

D

NTU = 1.50, epsilon = 0.777, T_c,out = 83.3°C

Test Your Knowledge

When rating an existing heat exchanger with known heat transfer area A and overall coefficient U under new operating inlet conditions, why is the Effectiveness-NTU method strictly preferred over the LMTD method?

A

The LMTD method violates the Second Law of Thermodynamics when applied to existing operating exchangers

B

The LMTD method requires iterative trial-and-error because the log mean temperature difference depends on unknown outlet temperatures, whereas Effectiveness-NTU calculates duty and outlet temperatures explicitly without iteration

C

The Effectiveness-NTU method is only valid when both fluid streams have matched heat capacity rates (C_r = 1.0)

D

The LMTD method cannot account for convective boundary layer resistances or fouling factors

Test Your Knowledge

Two process streams with matched heat capacity rates (C_h = C_c = 25.0 kW/K, so C_r = 1.0) enter a heat exchanger with a thermal size of NTU = 2.0. What is the thermal effectiveness epsilon for pure countercurrent flow versus pure parallel flow, and what is the theoretical maximum effectiveness achievable by each arrangement as NTU approaches infinity?

A

Countercurrent: epsilon = 0.500 (asymptote 0.500); Parallel: epsilon = 0.667 (asymptote 1.000)

B

Countercurrent: epsilon = 0.865 (asymptote 1.000); Parallel: epsilon = 0.632 (asymptote 0.800)

C

Countercurrent: epsilon = 0.667 (asymptote 1.000); Parallel: epsilon = 0.491 (asymptote 0.500)

D

Countercurrent: epsilon = 0.750 (asymptote 0.900); Parallel: epsilon = 0.333 (asymptote 0.500)

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