Introduction & Context

Moisture loss during blast freezing is a critical parameter in food process engineering, directly impacting product yield, quality, and shelf life. This calculation estimates the mass transfer of water vapor from the surface of an unpackaged food product to the surrounding high‑velocity air stream during the initial freezing phase. By quantifying the moisture loss, engineers can optimize freezer residence times, air velocities, and humidity levels to minimize dehydration (often referred to as “freezer burn” or “shrinkage”). For a deeper understanding of how freezing rate influences liquid exudate, see our drip loss prediction from freezing rate methodology, which complements this moisture‑loss analysis. This methodology is typically applied in the design and operational analysis of IQF (Individually Quick Frozen) tunnels and blast freezing chambers where the product surface remains in an active drying state.

Methodology & Formulas

The calculation relies on the Chilton-Colburn analogy to relate heat and mass transfer, assuming a Lewis number of unity. The process follows a sequential determination of fluid properties, flow regimes, and mass flux.

First, determine the film temperature Tf and the Reynolds number ReL to characterize the flow regime:

\[ T_{f} = \frac{T_{s} + T_{\infty}}{2} \] \[ Re_{L} = \frac{\rho \cdot U \cdot L}{\mu} \]

The Nusselt number NuL is selected based on the flow regime:

Regime Condition Formula
Laminar \( Re_{L} < 5 \times 10^{5} \) \( Nu_{L} = 0.664 \cdot Re_{L}^{0.5} \cdot Pr^{1/3} \)
Turbulent \( Re_{L} \geq 5 \times 10^{5} \) \( Nu_{L} = 0.037 \cdot Re_{L}^{0.8} \cdot Pr^{1/3} \)

The heat transfer coefficient h and the mass transfer coefficient hm are calculated as follows:

\[ h = \frac{Nu_{L} \cdot k}{L} \] \[ h_{m} = \frac{h}{\rho \cdot c_{p}} \]

The driving force for mass transfer is the difference in vapor density between the product surface and the bulk air, calculated using the ideal gas law:

\[ \rho_{v,\infty} = \frac{\phi_{\infty} \cdot P_{\mathrm{sat,ice}}(T_{\infty})}{R_{v} \cdot T_{\infty}} \] \[ \rho_{v,s} = \frac{P_{\mathrm{sat,ice}}(T_{s})}{R_{v} \cdot T_{s}} \] \[ \Delta\rho_{v} = \max(0, \rho_{v,s} - \rho_{v,\infty}) \]

Finally, the total mass loss mloss and the percentage weight loss are determined:

\[ \dot{m}'' = h_{m} \cdot \Delta\rho_{v} \] \[ m_{\mathrm{loss}} = \dot{m}'' \cdot A_{\mathrm{surf}} \cdot t_{\mathrm{active}} \] \[ \text{Loss}_{\%} = \left( \frac{m_{\mathrm{loss}}}{m_{\mathrm{initial}}} \right) \cdot 100 \]