Introduction & Context

Mixer type selection is a fundamental task in Process Engineering, ensuring that the mechanical energy provided by an impeller is effectively transferred to the fluid to achieve specific process objectives such as blending, solids suspension, or gas dispersion. Selecting the correct impeller geometry is critical to avoid inefficient power consumption, mechanical failure, or inadequate mixing performance.

This calculation is typically used during the design phase of stirred tank reactors or when scaling up processes from laboratory to industrial production. By characterizing the fluid regime through dimensionless numbers, engineers can match the impeller type to the fluid's physical properties and the required mixing intensity.

Methodology & Formulas

The selection process relies on calculating the Impeller Reynolds Number to determine the flow regime, followed by the application of Power Number correlations to estimate the energy requirements.

First, the rotational speed is converted from revolutions per minute to revolutions per second:

\[ n_rps = impeller_rpm / 60.0 \]

The fluid viscosity is converted from centipoise to Pascal-seconds:

\[ mu = mu_cp * 0.001 \]

The Impeller Reynolds Number (Re) is calculated to identify the flow regime:

\[ reynolds_number = (rho * n_rps * (impeller_diameter^2)) / mu \]

The Power Draw (P) is determined using the Power Number (Np), which varies based on the flow regime and impeller geometry:

\[ power_draw = np_val * rho * (n_rps^3) * (impeller_diameter^5) \]

Finally, the mixing intensity is evaluated by calculating the Power per Unit Volume:

\[ power_per_volume = power_draw / tank_volume \]
Flow Regime Reynolds Number (Re) Range Impeller Type Power Number (Np) Logic
Laminar Re < 10.0 Anchor np_val = 300.0 / reynolds_number
(Typical for anchor impellers)
Transitional 10.0 ≤ Re ≤ 10000.0 Pitched-Blade Turbine np_val = 1.5
(Approximate constant for 45° PBT; note: Np can vary with Re)
Turbulent Re > 10000.0 Rushton Turbine np_val = 5.0
(Typical constant for standard Rushton turbines)