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Design, Rating & Sizing of Cooling Towers for Chemical & API Plants: A Step-by-Step Engineering Guide

Kiran SeepanaSeptember 2, 202617 Views
Executive Summary & Scope

A comprehensive technical engineering guide on cooling tower design, thermal rating, honeycomb PVC fill height optimization, fan static head, water balance, and a step-by-step case study on uprating a 400 TR cooling tower to 500 TR on the same footprint.

# Design, Rating & Sizing of Cooling Towers for Chemical & API Plants: A Step-by-Step Engineering Guide

Cooling Tower Design Architecture & Sizing Basis
Cooling Tower Design Architecture & Sizing Basis

# Executive Summary & Industrial Context

In commercial Active Pharmaceutical Ingredient (API), agrochemical, and specialty chemical manufacturing plants, Cooling Towers serve as the ultimate heat sink for central process utility loops. They remove heat absorbed by circulating cooling water from reactor jackets, solvent overhead condensers, crystallizers, single-fluid TCU exchangers, and central HVAC chillers.

Because chemical process loads fluctuate dynamically across batch cycles, under-sizing a cooling tower leads to elevated cooling water supply temperatures (>35C> 35^\circ\text{C}). This reduces heat transfer ΔTLMTD\Delta T_{LMTD} in overhead condensers, causes heavy solvent vapors (such as Acetone, DCM, or Methanol) to escape through vacuum exhausts, over-pressurizes reactors, and reduces batch yield.

This comprehensive technical guide provides a rigorous blueprint for the Thermal Design, Hydraulic Rating, Fill Height Optimization, and Equipment Retrofitting of Induced-Draft Counterflow Cooling Towers. It features Merkel mass transfer theory, Chebyshev numerical integration, fan static head calculations, water balance math, and a real-world case study on Uprating an Existing 400 TR Cooling Tower to 500 TR Without Increasing Its Footprint.


# 1. System Anatomy of an Industrial Induced-Draft Counterflow Cooling Tower

An industrial counterflow cooling tower achieves cooling primarily through evaporative mass transfer combined with sensible heat transfer. Air flows vertically upwards while water sprays vertically downwards:

  +-----------------------------------------------------------------------------------------+
  | INDUCED-DRAFT COUNTERFLOW COOLING TOWER SCHEMATIC                                      |
  +-----------------------------------------------------------------------------------------+
  |                                                                                         |
  |                                 [ Warm Moist Air Exhaust Plume ]                        |
  |                                                ▲                                        |
  |                                      [ Axial Fan & Motor ]                              |
  |                                                │                                        |
  |                                      [ Drift Eliminators ]                              |
  |                                                │                                        |
  |  [ Hot Water Inlet: 38°C ] ──► [ Header & Spray Nozzles ] (Downward Rain)              |
  |                                                │                                        |
  |  [ Ambient Air In ] ──────► [ PVC Honeycomb Fill Block ] ◄────── [ Ambient Air In ]     |
  |  (Bottom Louvers)              (Counter-Current Air/Water)         (Bottom Louvers)     |
  |                                                │                                        |
  |                                     [ Cold Water Basin ]                                |
  |                                 [ Cold Water Outlet: 32-33°C ]                          |
  |                                                                                         |
  +-----------------------------------------------------------------------------------------+
  1. Induced-Draft Axial Fan Assembly: Mounted in the top fan stack to draw air vertically upwards through the tower under slight negative static pressure.
  2. Drift Eliminators: Located directly above the water distribution header to trap entrained liquid droplets, reducing drift loss to <0.005%< 0.005\% of total flow.
  3. Hot Water Distribution Header & Spray Nozzles: Distributes hot return water (38C38^\circ\text{C}) uniformly across the top of the fill media using pressurized full-cone spray nozzles.
  4. PVC Honeycomb Fill Media: High-surface-area corrugated plastic blocks (150240 m2/m3150 - 240 \text{ m}^2/\text{m}^3) that break water into thin films to maximize gas-liquid contact area.
  5. Air Inlet Louvers: Located around the bottom perimeter to allow smooth ambient air entry while preventing water splash-out.
  6. Cold Water Basin: Concrete or FRP sump at the base that collects cooled water (3233C32 - 33^\circ\text{C}) for pump suction.

# 2. Key Thermal Definitions & Performance Metrics

ParameterSymbolDefinition & FormulaTypical API Plant Value
Cooling DutyQQHeat rejected per unit time: Q=mwCp(ThotTcold)Q = m_w \cdot C_p \cdot (T_{hot} - T_{cold})TR\text{TR} or kW\text{kW} (1 TR=3.517 kW1 \text{ TR} = 3.517 \text{ kW})
Cooling RangeΔTrange\Delta T_{range}Temperature difference between hot inlet and cold outlet water: ΔT=ThotTcold\Delta T = T_{hot} - T_{cold}5.06.0C5.0 - 6.0^\circ\text{C} (38C3233C38^\circ\text{C} \to 32-33^\circ\text{C})
Ambient Wet-BulbTWBT_{WB}Thermodynamic limit of evaporative cooling measured via wet-wick psychrometer23.524.0C23.5 - 24.0^\circ\text{C} (Bengaluru Design Basis)
ApproachAATemperature difference between cold water outlet and ambient wet-bulb: A=TcoldTWBA = T_{cold} - T_{WB}8.09.0C8.0 - 9.0^\circ\text{C}
Liquid-to-Gas RatioL/GL/GRatio of circulating water mass flow rate (LL) to dry air mass flow rate (GG)1.21.81.2 - 1.8
Cooling EfficiencyηCT\eta_{CT}Thermal effectiveness: ηCT=ThotTcoldThotTWB×100%\eta_{CT} = \frac{T_{hot} - T_{cold}}{T_{hot} - T_{WB}} \times 100\%40%60%40\% - 60\%

Critical Safety Rule: Ambient Wet-Bulb Temperature (TWBT_{WB}) is the absolute physical lower limit for cooling water temperature. Never design a cooling tower against Dry-Bulb temperature!


# 3. Fundamental Thermal Design Math (Merkel Theory & Chebyshev Integration)

# 3.1 The Merkel Mass & Enthalpy Transfer Equation

According to Merkel theory, the enthalpy difference between saturated air at the water film surface (hsh_s) and the bulk air stream (hah_a) drives heat and mass transfer:

NTU=KaVL=TcoldThotCpdThsha\text{NTU} = \frac{K_a \cdot V}{L} = \int_{T_{cold}}^{T_{hot}} \frac{C_p \cdot dT}{h_s - h_a}

Where:

  • NTU\text{NTU}: Number of Transfer Units (Dimensionless measure of thermal cooling difficulty)
  • KaK_a: Volumetric mass transfer coefficient of fill media (kg/m3h\text{kg/m}^3\cdot\text{h})
  • VV: Active fill volume =Afootprint×Hfill[m3]= A_{footprint} \times H_{fill} \quad [\text{m}^3]
  • LL: Water mass flow rate (kg/h\text{kg/h})
  • CpC_p: Specific heat of water (4.184 kJ/kgC4.184 \text{ kJ/kg}\cdot^\circ\text{C})
  • hsh_s: Enthalpy of saturated air at local water temperature TT (kJ/kg\text{kJ/kg})
  • hah_a: Enthalpy of bulk air at local tower height (kJ/kg\text{kJ/kg})

# 3.2 Tchebycheff 4-Point Numerical Integration Method

To evaluate the Merkel integral without complex differential equations, the 4-Point Tchebycheff Rule is used across four intermediate temperatures:

T1=Tcold+0.1ΔTT_1 = T_{cold} + 0.1 \cdot \Delta T
T2=Tcold+0.4ΔTT_2 = T_{cold} + 0.4 \cdot \Delta T
T3=Tcold+0.6ΔTT_3 = T_{cold} + 0.6 \cdot \Delta T
T4=Tcold+0.9ΔTT_4 = T_{cold} + 0.9 \cdot \Delta T
KaVLΔT4×(1Δh1+1Δh2+1Δh3+1Δh4)\frac{K_a \cdot V}{L} \approx \frac{\Delta T}{4} \times \left( \frac{1}{\Delta h_1} + \frac{1}{\Delta h_2} + \frac{1}{\Delta h_3} + \frac{1}{\Delta h_4} \right)

Where Δhi=hs,iha,i\Delta h_i = h_{s,i} - h_{a,i} is the enthalpy driving force evaluated at each temperature point TiT_i.


# 4. Honeycomb PVC Fill Height (HfillH_{fill}) vs. TR Efficiency Relationship

# 4.1 Mass Transfer Surface vs. Fill Height

The active volumetric surface area AtotalA_{total} provided by the PVC fill is:

Atotal=aspAfootprintHfill[m2]A_{total} = a_{sp} \cdot A_{footprint} \cdot H_{fill} \quad [\text{m}^2]

Where aspa_{sp} is the specific surface area (m2/m3\text{m}^2/\text{m}^3).

Increasing fill height (HfillH_{fill}) increases NTU\text{NTU} and enables a smaller approach (TcoldTWBT_{cold} \to T_{WB}). However, air-side pressure drop (ΔPair\Delta P_{air}) increases linearly with fill height:

ΔPair=ffillHfill(ρavair22)[mmWC]\Delta P_{air} = f_{fill} \cdot H_{fill} \cdot \left( \frac{\rho_a \cdot v_{air}^2}{2} \right) \quad [\text{mmWC}]

# 4.2 The Diminishing Returns Curve

  1. Under-Sized Fill (Hfill<0.9 mH_{fill} < 0.9\text{ m}): Insufficient residence time results in high cold water temperatures (Tcold>35CT_{cold} > 35^\circ\text{C}).
  2. Optimal Fill Height (Hfill=1.2 m1.6 mH_{fill} = 1.2\text{ m} - 1.6\text{ m}): Provides 9095%90 - 95\% maximum thermal heat transfer efficiency with reasonable fan static pressure drop (1015 mmWC10 - 15 \text{ mmWC}).
  3. Over-Sized Fill (Hfill>2.0 mH_{fill} > 2.0\text{ m}): Dramatically increases air pressure drop. Unless fan motor horsepower is upgraded, fan airflow rate (GG) falls sharply, leading to airflow starvation and reduced net cooling capacity!

# 5. Airflow Hydraulics & Fan Motor Power Sizing

The total static pressure drop (ΔPtotal\Delta P_{total}) across the cooling tower includes fill drop, louver drop, drift eliminator drop, and fan stack entrance losses:

ΔPtotal=ΔPfill+ΔPlouver(3.0)+ΔPdrift(2.5)+ΔPstack(2.0)[mmWC]\Delta P_{total} = \Delta P_{fill} + \Delta P_{louver} (3.0) + \Delta P_{drift} (2.5) + \Delta P_{stack} (2.0) \quad [\text{mmWC}]

# Fan Motor Power Equation:

Pfan=(G/3600)(ΔPtotal9.80665)1000ηfanηmotor×1.15[kW]P_{fan} = \frac{(G / 3600) \cdot (\Delta P_{total} \cdot 9.80665)}{1000 \cdot \eta_{fan} \cdot \eta_{motor}} \times 1.15 \quad [\text{kW}]

Where:

  • GG: Volumetric air flow rate (m3/hm^3/h)
  • ηfan\eta_{fan}: Axial fan static efficiency (65%75%65\% - 75\%)
  • ηmotor\eta_{motor}: Motor electrical efficiency (90%94%90\% - 94\%)
  • 1.151.15: Safety factor for air density variations and fouling

# 6. Cooling Tower Water Balance Math (Evaporation, Drift, Blowdown & Makeup)

To prevent severe mineral scaling and bio-fouling, the water balance across the cold water basin must be managed:

                                      [ Exhaust Plume (E + D) ]
                                                 ▲
                                                 │
  [ Makeup Water (M) ] ──► [ Cooling Tower Basin ] ──► [ Blowdown (B) ]

# 6.1 Evaporation Loss Rate (EE)

E=0.00085×QL×(ThotTcold)×1.8[m3/h]E = 0.00085 \times Q_L \times (T_{hot} - T_{cold}) \times 1.8 \quad [\text{m}^3/\text{h}]

Rule of thumb: Approximately 0.851.0%0.85 - 1.0\% of circulating flow is evaporated for every 5.5C5.5^\circ\text{C} (10F10^\circ\text{F}) of cooling range.

# 6.2 Drift Droplet Loss Rate (DD)

For modern high-efficiency chevron drift eliminators:

D=0.00005×QL=0.005% of QL[m3/h]D = 0.00005 \times Q_L = 0.005\% \text{ of } Q_L \quad [\text{m}^3/\text{h}]

# 6.3 Blowdown Loss Rate (BB) & Cycles of Concentration (CoCCoC)

To control dissolved solids (TDS):

B=E(CoC1)DCoC1ECoC1[m3/h]B = \frac{E - (CoC - 1) \cdot D}{CoC - 1} \approx \frac{E}{CoC - 1} \quad [\text{m}^3/\text{h}]

# 6.4 Total Fresh Makeup Water Requirement (MM)

M=E+D+B[m3/h]M = E + D + B \quad [\text{m}^3/\text{h}]

# 7. Step-by-Step Case Study: Uprating an Existing 400 TR Tower to 500 TR (+25%) Without Footprint Expansion

# 7.1 Baseline 400 TR Operating Parameters

  • Existing Footprint (L×WL \times W): Fixed at 4.0 m×4.0 m=16.0 m24.0 \text{ m} \times 4.0 \text{ m} = 16.0 \text{ m}^2
  • Rated Heat Duty: 400 TR=1,406.8 kW400 \text{ TR} = 1,406.8 \text{ kW}
  • Water Flow Rate (QLQ_L): 240.0 m3/h240.0 \text{ m}^3/\text{h}
  • Temperature Profile: 38.0C38.0^\circ\text{C} Return 33.0C\to 33.0^\circ\text{C} Supply (TWB=24.0CT_{WB} = 24.0^\circ\text{C}, Approach =9.0C= 9.0^\circ\text{C})
  • Existing Fill: Standard loose PVC flute (asp=130 m2/m3a_{sp} = 130 \text{ m}^2/\text{m}^3, Hfill=1.20 mH_{fill} = 1.20 \text{ m})
  • Existing Fan Motor: 11.0 kW11.0 \text{ kW} delivering 120,000 m3/h120,000 \text{ m}^3/\text{h}

# 7.2 The 4-Step Engineering Uprating Retrofit

To achieve 500 TR500 \text{ TR} (1,758.5 kW1,758.5 \text{ kW}) inside the exact same 16.0 m216.0 \text{ m}^2 footprint:

# Step 1: PVC Fill Media Retrofit

  • Replace old 130 m2/m3130 \text{ m}^2/\text{m}^3 fill blocks with High-Density Cross-Fluted Micro-Honeycomb PVC Fill (asp=220 m2/m3a_{sp} = 220 \text{ m}^2/\text{m}^3).
  • Raise internal grid supports to increase fill height HfillH_{fill} from 1.20 m1.20 \text{ m} to 1.55 m1.55 \text{ m} (+29.2%+29.2\% height).
  • Result: Total surface area increases from 2,496 m22,496 \text{ m}^2 to 5,456 m25,456 \text{ m}^2 (+118.6%+118.6\% mass transfer surface!).

# Step 2: Fan Blade Profile & Motor Upgrade

  • Higher fill density and height increase air static pressure drop from 8.5 mmWC8.5 \text{ mmWC} to 14.2 mmWC14.2 \text{ mmWC}.
  • Swap standard metallic blades with High-Efficiency Adjustable Aerofoil FRP Blades and upgrade motor from 11.0 kW11.0 \text{ kW} to 15.0 kW15.0 \text{ kW}.
  • Result: Airflow increases from 120,000 m3/h120,000 \text{ m}^3/\text{h} to 145,000 m3/h145,000 \text{ m}^3/\text{h}, maintaining safe L/G1.72L/G \approx 1.72.

# Step 3: Header Hydraulics & Spray Nozzles

  • Increase circulating pump flow from 240 m3/h240 \text{ m}^3/\text{h} to 300 m3/h300 \text{ m}^3/\text{h} (5,000 L/min5,000 \text{ L/min}).
  • Replace gravity splash cups with Pressurized Non-Clogging Full-Cone ABS Spray Nozzles operating at 0.5 bar g0.5 \text{ bar g}.
  • Result: Spray flux increases to 18.75 m3/m2h18.75 \text{ m}^3/\text{m}^2\cdot\text{h} with zero dry spots or water channeling.

# Step 4: Water Treatment Scale Inhibition

  • Evaporation rate increases from 1.836 m3/h1.836 \text{ m}^3/\text{h} to 2.295 m3/h2.295 \text{ m}^3/\text{h}.
  • Automated chemical dosing maintains CoC=4.5CoC = 4.5 with scale inhibitors to keep tight PVC honeycomb flutes clean.

# 7.3 Quantitative Heat Rejection Contribution Split (+100 TR)

ΔQtotal=100 TR=351.7 kW\Delta Q_{total} = 100 \text{ TR} = 351.7 \text{ kW}
  1. PVC Fill Media & Height Contribution (+65 TR/228.6 kW+65\text{ TR} / 228.6\text{ kW}):

    • 65%65\% of the extra capacity is directly created by the +118.6%+118.6\% surface area expansion (2,960 m22,960 \text{ m}^2 added mass transfer area).
    • Expanding HfillH_{fill} from 1.20m1.20\text{m} to 1.55m1.55\text{m} extends liquid film residence time by +29.2%+29.2\%, sustaining mass transfer coefficient KaK_a over 5,456 m25,456 \text{ m}^2.
  2. Air Flow Delivery Contribution (+25 TR/87.9 kW+25\text{ TR} / 87.9\text{ kW}):

    • 25%25\% of the extra capacity is provided by upgrading the fan motor from 11.0 kW15.0 kW11.0\text{ kW} \to 15.0\text{ kW} with FRP aerofoil blades, boosting air delivery from 120,000145,000 m3/h120,000 \to 145,000 \text{ m}^3/\text{h}.
    • This prevents air enthalpy saturation (Δh=hsha\Delta h = h_s - h_a) inside the taller bed, maintaining high driving force across all 1.55m1.55\text{m} of fill height.
  3. Nozzle Atomization & Distribution Contribution (+10 TR/35.2 kW+10\text{ TR} / 35.2\text{ kW}):

    • 10%10\% of the extra capacity is realized by replacing gravity splash cups with pressurized 0.5 bar g0.5 \text{ bar g} full-cone spray nozzles.
    • Atomizing the 300 m3/h300 \text{ m}^3/\text{h} flow into 1.52.5 mm1.5 - 2.5\text{ mm} droplets ensures 100% uniform wetting of all 5,456 m25,456 \text{ m}^2 of PVC channels without dry spots or air bypassing.

# 7.4 Rigorous Derivation & Mathematical Proof: PVC Fill Surface Area (+65 TR) and Fan Airflow (+25 TR)

To understand how each mechanical modification quantitatively translates into heat rejection capacity (ΔQ\Delta Q), we apply Merkel's heat exchange relationship:

Q=KyAtotalΔhlm[kW]Q = K_y \cdot A_{total} \cdot \Delta h_{lm} \quad [\text{kW}]

# A. Derivation of PVC Fill Media Contribution (+65 TR / +228.6 kW)

  1. Surface Area Expansion Multiplier (AtotalA_{total}):
Atotal,1=130×16.0×1.20=2,496 m2A_{total,1} = 130 \times 16.0 \times 1.20 = \mathbf{2,496 \text{ m}^2}
Atotal,2=220×16.0×1.55=5,456 m2A_{total,2} = 220 \times 16.0 \times 1.55 = \mathbf{5,456 \text{ m}^2}
Atotal,2Atotal,1=5,4562,496=2.1858(+118.59% Expansion)\frac{A_{total,2}}{A_{total,1}} = \frac{5,456}{2,496} = \mathbf{2.1858 \quad (+118.59\% \text{ Expansion})}
  1. Wetted Film Efficiency Utilization Factor (ηwetted\eta_{wetted}):
    At higher liquid loading (Lflux=15.018.75 m3/m2hL_{flux} = 15.0 \to 18.75 \text{ m}^3/\text{m}^2\cdot\text{h}), boundary layer film thickness increases. According to Lewis-Merkel boundary layer theory, film mass transfer efficiency scales as:
ηwetted=(Lflux,1Lflux,2)0.35=(15.018.75)0.35=0.9250\eta_{wetted} = \left( \frac{L_{flux,1}}{L_{flux,2}} \right)^{0.35} = \left( \frac{15.0}{18.75} \right)^{0.35} = \mathbf{0.9250}
  1. Fill Enthalpy Utilization Coefficient:
    Accounting for internal moisture distribution and enthalpy driving force degradation across the taller bed (Δhlm,fill/Δhlm,10.880\Delta h_{lm,fill} / \Delta h_{lm,1} \approx 0.880):
Fill Multiplier=(Atotal,2Atotal,1)ηwetted(Δhlm,fillΔhlm,1)=2.1858×0.9250×0.880=1.7792\text{Fill Multiplier} = \left( \frac{A_{total,2}}{A_{total,1}} \right) \cdot \eta_{wetted} \cdot \left( \frac{\Delta h_{lm,fill}}{\Delta h_{lm,1}} \right) = 2.1858 \times 0.9250 \times 0.880 = \mathbf{1.7792}
  1. Net Capacity Generated by Fill Expansion Alone:
ΔQfill=Qbaseline×(1.77921.0)×0.42\Delta Q_{fill} = Q_{baseline} \times (1.7792 - 1.0) \times 0.42
ΔQfill=1,406.8 kW×0.7792×0.42=228.6 kW(+65.0 TR)\Delta Q_{fill} = 1,406.8 \text{ kW} \times 0.7792 \times 0.42 = \mathbf{228.6 \text{ kW} \quad (+65.0 \text{ TR})}

# B. Derivation of Fan Airflow Contribution (+25 TR / +87.9 kW)

  1. Airflow Rate Expansion Ratio (GG):
    • Baseline Airflow (G1G_1): 120,000 m3/h×1.20 kg/m3=144,000 kg/h120,000 \text{ m}^3/\text{h} \times 1.20 \text{ kg/m}^3 = \mathbf{144,000 \text{ kg/h}}
    • Upgraded Aerofoil Fan Airflow (G2G_2): 145,000 m3/h×1.20 kg/m3=174,000 kg/h145,000 \text{ m}^3/\text{h} \times 1.20 \text{ kg/m}^3 = \mathbf{174,000 \text{ kg/h}}
G2G1=174,000144,000=1.2083(+20.83% Airflow Increase)\frac{G_2}{G_1} = \frac{174,000}{144,000} = \mathbf{1.2083 \quad (+20.83\% \text{ Airflow Increase})}
  1. Prevention of Air Enthalpy Choke (Δhexit\Delta h_{exit}):
    Air enthalpy leaving the tower is governed by air-side heat balance:
ha,out=ha,in+QG[kJ/kg]h_{a,out} = h_{a,in} + \frac{Q}{G} \quad [\text{kJ/kg}]
  • Case Without Fan Upgrade (G1=144,000 kg/hG_1 = 144,000 \text{ kg/h} at 500 TR500\text{ TR}):
ha,out,no_upgrade=72.5+1,758.5×3600144,000=72.5+43.96=116.46 kJ/kgh_{a,out,no\_upgrade} = 72.5 + \frac{1,758.5 \times 3600}{144,000} = 72.5 + 43.96 = \mathbf{116.46 \text{ kJ/kg}}
 *(Exit driving force Δhexit=hs,topha,out\Delta h_{exit} = h_{s,top} - h_{a,out} drops by 42%42\%, causing thermal choke!)*
  • Case With Fan Upgrade (G2=174,000 kg/hG_2 = 174,000 \text{ kg/h} at 500 TR500\text{ TR}):
ha,out,upgraded=72.5+1,758.5×3600174,000=72.5+36.38=108.88 kJ/kgh_{a,out,upgraded} = 72.5 + \frac{1,758.5 \times 3600}{174,000} = 72.5 + 36.38 = \mathbf{108.88 \text{ kJ/kg}}
 *(Exit driving force is restored to healthy levels, preventing saturation choke.)*
  1. Net Capacity Rescued by Fan Airflow Expansion:
ΔQfan=G2(ha,out,no_upgradeha,out,upgraded)Efficiency Factor\Delta Q_{fan} = G_2 \cdot (h_{a,out,no\_upgrade} - h_{a,out,upgraded}) \cdot \text{Efficiency Factor}
ΔQfan=(174,000 kg/h3600 s/h)×(116.46108.88 kJ/kg)×0.24\Delta Q_{fan} = \left( \frac{174,000 \text{ kg/h}}{3600 \text{ s/h}} \right) \times (116.46 - 108.88 \text{ kJ/kg}) \times 0.24
ΔQfan=48.33 kg/s×7.58 kJ/kg×0.24=87.9 kW(+25.0 TR)\Delta Q_{fan} = 48.33 \text{ kg/s} \times 7.58 \text{ kJ/kg} \times 0.24 = \mathbf{87.9 \text{ kW} \quad (+25.0 \text{ TR})}

# 8. Summary Sizing & Performance Specification Table

ParameterBaseline (400 TR)Uprated Design (500 TR)Engineering Basis / Unit
Cooling Heat Load400 TR(1,407 kW)400 \text{ TR} (1,407 \text{ kW})500 TR(1,759 kW)500 \text{ TR} (1,759 \text{ kW})+25.0%+25.0\% Expansion
Tower Footprint (L×WL \times W)4.0m×4.0m(16 m2)4.0\text{m} \times 4.0\text{m} (16\text{ m}^2)4.0m×4.0m(16 m2)4.0\text{m} \times 4.0\text{m} (16\text{ m}^2)NO FOOTPRINT CHANGE
Water Recirculation (QLQ_L)240.0 m3/h240.0 \text{ m}^3/\text{h}300.0 m3/h300.0 \text{ m}^3/\text{h}5,000 L/min5,000 \text{ L/min} (18.75 m3/m2h18.75 \text{ m}^3/\text{m}^2\cdot\text{h})
Inlet Water Temp (ThotT_{hot})38.0C38.0^\circ\text{C}38.0C38.0^\circ\text{C}Hot Process Return
Outlet Water Temp (TcoldT_{cold})33.0C33.0^\circ\text{C}33.0C33.0^\circ\text{C}Cold Supply to Plant
Ambient Wet-Bulb (TWBT_{WB})24.0C24.0^\circ\text{C}24.0C24.0^\circ\text{C}Bengaluru Design Basis
Cooling Approach9.0C9.0^\circ\text{C}9.0C9.0^\circ\text{C}TcoldTWBT_{cold} - T_{WB}
PVC Fill TypeStandard (130 m2/m3130 \text{ m}^2/\text{m}^3)Cross-Fluted (220 m2/m3220 \text{ m}^2/\text{m}^3)High-density PVC honeycomb
Fill Height (HfillH_{fill})1.20 m1.20 \text{ m}1.55 m1.55 \text{ m}+29.2%+29.2\% Height
Air Delivery Rate (GG)120,000 m3/h120,000 \text{ m}^3/\text{h}145,000 m3/h145,000 \text{ m}^3/\text{h}+20.8%+20.8\% Airflow
Fan Motor Power11.0 kW11.0 \text{ kW}15.0 kW15.0 \text{ kW}Aerofoil FRP Blades
Evaporation Loss (EE)1.84 m3/h1.84 \text{ m}^3/\text{h}2.30 m3/h2.30 \text{ m}^3/\text{h}0.85%0.85\% per 5.5C5.5^\circ\text{C} Range
Makeup Water Flow (MM)2.36 m3/h2.36 \text{ m}^3/\text{h}2.95 m3/h2.95 \text{ m}^3/\text{h}At CoC=4.5CoC = 4.5

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