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Reynolds Analogy & Chilton-Colburn J-Factor Calculator

The Reynolds analogy and its empirical refinement, the Chilton-Colburn analogy, establish a powerful mathematical bridge linking momentum boundary layer friction to convective heat and mass transfer.

Dimensionless wall shear friction coefficient (tau_w / (0.5 * rho * U^2)).

Momentum-to-thermal diffusivity ratio (0.71 for air, ~6 for water).

Momentum-to-mass diffusivity ratio (0.6 for water vapor in air).

Calculated Result
0.00250

Colburn j-Factor (j_H = j_M)

Heat Transfer Stanton Number (St_H)

0.00314

Friction Analogy: C_f / 2

0.00250

Prandtl / Schmidt Numbers

Pr = 0.71, Sc = 0.6

Calculation Breakdown

  1. j_H = C_f / 20.005 / 2 = 0.00250
  2. St_H = j_H / Pr^(2/3)0.00314

What Is the Reynolds Analogy & Chilton-Colburn J-Factor Calculator?

The Chilton-Colburn analogy extends the classical Reynolds analogy (valid only for Pr = 1) to fluids with arbitrary Prandtl and Schmidt numbers (0.6 < Pr < 60).

It asserts that dimensionless momentum transfer, heat transfer, and mass transfer follow identical governing boundary layer equations.

How Does the Reynolds Analogy & Chilton-Colburn J-Factor Calculator Work?

Evaluates the Colburn j-factor: j_H = j_M = Cf / 2.

Computes the heat transfer Stanton number: St_H = j_H / Pr^(2/3).

Evaluates mass transfer Stanton number.

Reynolds Analogy & Chilton-Colburn J-Factor Calculator Formula & Variables

The core mathematical equation utilized by this calculator is expressed as:

j_H = \text{St}_H \cdot \text{Pr}^{2/3} = \frac{C_f}{2}, \quad j_M = \text{St}_M \cdot \text{Sc}^{2/3} = \frac{C_f}{2}, \quad \text{St} = \frac{h}{\rho C_p U}

Chilton-Colburn analogy relating friction coefficient to heat and mass transfer Stanton numbers.

How to Use the Reynolds Analogy & Chilton-Colburn J-Factor Calculator

  1. Enter the skin friction coefficient Cf (or Moody friction factor / 4).
  2. Enter the Prandtl number of the fluid.
  3. Enter the Schmidt number for mass transfer.

Step-by-Step Example Calculation

Turbulent Pipe Flow Air Cooling

Input Values:

skinFrictionCoefficientCf:0.005
prandtlNumberPr:0.71
schmidtNumberSc:0.6
Worked Steps: Predicting heat transfer Stanton number from pressure drop friction factor in a duct.

Understanding Your Result

The Stanton number represents the ratio of heat transferred into a fluid to the thermal capacity of the fluid.

Higher skin friction generally implies proportionally higher convective heat transfer.

Factors That Affect the Result

  • Prandtl number: In high-Pr fluids (heavy oils), the thermal boundary layer is much thinner than the velocity boundary layer.
  • Surface roughness: Turbulence promoters increase both heat transfer and pressure drop, but can disrupt exact analogy scaling.

When Should You Use This Calculator?

  • Predicting heat exchanger performance from pressure drop measurements.
  • Evaporative cooling, psychrometrics, and drying processes linking heat and moisture transfer.

Assumptions & Limitations

  • Valid for attached turbulent boundary layers without separation or adverse pressure gradients.
  • Applicable for 0.6 < Pr < 60 and 0.6 < Sc < 3000.

Frequently Asked Questions

Calculation Accuracy & Reference Note

Standard transport analogy supported by extensive chemical and mechanical engineering data.

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