For water-based heat exchanger experiments, a widely used simplified equation for the tube‑side heat transfer coefficient is (h_i = \frac{4200,(1.35 + 0.02,t),u_i^{0.8}}{d_i^{0.2}}). Here (h_i) is in (\text{W}/(\text{m}^2!\cdot!^\circ\text{C})), (t) is the average water temperature in (^\circ\text{C}), (u_i) the water velocity in (\text{m}/\text{s}), and (d_i) the tube inner diameter in millimetres. This single expression lets you bypass property tables and directly compute the film coefficient from only temperature, velocity and diameter – a deliberate shortcut for educational pilot‑plant work.
Core takeaway: The formula embeds the temperature‑dependent physical properties of water into one compact relation, making it ideal for quick, repeatable student calculations. It sacrifices some accuracy for speed, so it must be used within its intended range – fully turbulent flow, moderate temperatures, and no phase change.
Why the Equation Exists
From General Correlation to Water‑Only Shortcut
All forced‑convection heat transfer coefficients for smooth tubes are rooted in the Dittus‑Boelter (or Sieder‑Tate) correlation: [ Nu = 0.023,Re^{0.8}Pr^{n} ] where (Nu = \frac{h_i d_i}{k}), (Re = \frac{\rho u_i d_i}{\mu}), and (Pr = \frac{c_p \mu}{k}).
For water, density, viscosity, thermal conductivity and specific heat are all strong functions of temperature. By substituting empirical fits for these properties over the 0–100 °C range, the dimensional constants collapse into a form that depends only on velocity, diameter, and average temperature. The numerator (4200(1.35 + 0.02,t)) captures the temperature‑sensitive group (\rho^{0.8} c_p^{0.4} k^{0.6} \mu^{-0.4}), while the (u_i^{0.8}/d_i^{0.2}) fragment directly mirrors the Reynolds‑and‑Prandtl scaling of turbulent flow.
The Role of the Empirical Constants
- 4200: a dimensional conversion factor that also absorbs the typical magnitude of water’s properties in SI units.
- 1.35 + 0.02 t: a linearised correction that adjusts for the change in the property group with temperature; at 25 °C the factor becomes 1.85, matching well‑known water data.
- Exponents 0.8 and -0.2: inherited from the fully‑developed turbulent flow regime ((Re > 10^4)), where the Nusselt number scales with (Re^{0.8}) and is nearly independent of tube length.
How to Use It in a Pilot‑Plant Setting
Step‑by‑Step Variable Definition
- (u_i): Calculate from the measured volumetric flow rate (V) (m³/s) and the tube cross‑sectional area based on inner diameter (d_i): (u_i = \frac{4V}{\pi d_i^2}) (with (d_i) in metres for velocity).
- (d_i): Use the inner diameter in millimetres. This is the deliberate quirk of the formula – if you use metres, the answer will be wrong by three orders of magnitude.
- (t): The arithmetic mean of the inlet and outlet water temperatures. Quick probe readings are sufficient; the formula tolerates a few degrees of uncertainty.
Checking Your Result
The output (h_i) will typically fall between 2000 and 15 000 W/(m²·°C) for water flowing at 0.5–3 m/s in 10–25 mm tubes. If your computed value is outside this range, re‑check the diameter unit (millimetres!) or confirm that the flow is fully turbulent and no boiling is occurring.
Connecting to Overall Heat Transfer
In a pilot‑plant experiment, this (h_i) feeds directly into the overall heat transfer coefficient (U_o): [ \frac{1}{U_o} = \frac{1}{h_o} + \frac{1}{h_{od}} + \frac{d_o \ln(d_o/d_i)}{2k_w} + \frac{d_o}{d_i}\frac{1}{h_{id}} + \frac{d_o}{d_i}\frac{1}{h_i} ]
Students often measure the overall (U) experimentally via (Q = U A \Delta T_m) and then back‑calculate the tube‑side film coefficient by subtracting the known thermal resistances of the wall, fouling, and shell side. The simplified (h_i) formula serves as a rapid independent check – any large discrepancy points to measurement errors, unexpected fouling, or departure from the formula’s underlying assumptions.
Where the Simplified Equation Falls Short
Flow Regime and Temperature Limits
The formula assumes fully turbulent flow ((Re > 10^4)). In the transition region (2300–10 000) or laminar flow, the 0.8 exponent is invalid, and the calculated (h_i) will be far too high.
It is built for liquid water between roughly 0 and 100 °C. Below freezing or near the boiling point, the linear property correction (1.35 + 0.02t) loses accuracy. If the water contains glycol or other additives, the underlying property values are different and the equation is no longer valid.
Missing Viscosity Correction
General correlations often include a term ((\mu/\mu_w)^{0.14}) to account for the difference between bulk fluid viscosity and the viscosity at the tube wall. The simplified formula omits this correction, assuming the wall temperature is close to the bulk fluid temperature. When large temperature differences exist (e.g., steam heating water where the wall is much hotter), the real (h_i) can differ by 10–20 %. In rigorous design work, you would revert to the full Sieder‑Tate equation with property evaluation at the film temperature.
Limited to Clean, Straight Tubes
The formula applies to smooth, straight tubes with fully developed hydrodynamic and thermal boundary layers. Entrance effects, coiled tubes, or internally finned tubes change the exponent and the constant. Likewise, any fouling layer is not accounted for; the equation gives the clean‑surface coefficient, and students must add a separate fouling resistance ((1/h_{id})) as shown in the overall resistance network.
Common Pitfalls When Using This Shortcut
Unit Confusion
The most frequent mistake is entering the inner diameter in metres. The constant 4200 was derived assuming (d_i) in mm. If you use 0.015 m for a 15 mm tube, the denominator (d_i^{0.2}) becomes 0.015⁰·² ≈ 0.43 instead of 15⁰·² ≈ 1.72, giving a coefficient that is four times too large.
Applying the Formula Outside Water Systems
The property‑lumping is exclusive to water. For any other fluid – even a 50 % water–glycol mixture – the constants 4200 and the temperature factor 1.35 + 0.02t are meaningless. You must return to the fundamental (Nu = f(Re, Pr)) correlation and evaluate properties individually.
Forgetting That It’s a Film Coefficient, Not (U)
A frequent student error is to treat (h_i) as the overall heat transfer coefficient. The tube‑side film coefficient is just one thermal resistance in a series; the overall (U) will always be lower, sometimes significantly so if the shell‑side or fouling resistances are dominant.
Matching the Right Approach to Your Goal
- If your primary focus is a quick, repeatable educational comparison of water‑side performance: Use the simplified formula directly. It lets you spend lab time on experimental technique rather than property look‑ups, while still showing the correct velocity and diameter dependence.
- If your primary focus is accurate design or troubleshooting of an industrial water heater/cooler: Discard the simplified equation. Instead, use the full Sieder‑Tate correlation with property data at the film temperature and include the viscosity ratio correction.
- If the experiments involve significant temperature differences, boiling, or viscous fluids: The simplified water equation is not safe. Derive (h_i) from the fundamental Nusselt‑number relation and always apply the ((\mu/\mu_w)^{0.14}) correction.
- If you need to teach the why behind the shortcut: Ask students to calculate (h_i) both ways – with the simplified formula and by evaluating water properties at the average temperature and solving (Nu = 0.023 Re^{0.8} Pr^{0.4}). The agreement (typically within ±5 %) reinforces the physics while making the shortcut’s origin tangible.
The simple empirical equation turns a multi‑step, table‑laden calculation into a one‑line estimate. When you understand its boundaries, it becomes a powerful teaching and field‑diagnostic tool – one that bridges abstract correlation theory and practical, hands‑on heat exchanger experiments.
Summary Table:
| Variable | Description | Unit | Key Constraint / Notes |
|---|---|---|---|
| $h_i$ | Tube-side heat transfer coefficient | W/(m²·°C) | Output calculation result |
| $t$ | Average water temperature | °C | Arithmetic mean of inlet and outlet |
| $u_i$ | Water velocity | m/s | Flow must be fully turbulent ($Re > 10^4$) |
| $d_i$ | Tube inner diameter | mm | Must be entered in millimeters (not meters) |
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