Introduction & Context

Tangential flow minimisation is a key design objective in mechanically agitated vessels used throughout the process industries (pharmaceutical, biochemical, water treatment, petrochemical, food & beverage). Excessive swirl reduces axial turnover, lowers gas–liquid mass-transfer rates, promotes vortexing and air entrainment, and wastes mechanical energy. The worksheet quantifies the residual tangential velocity after standard wall baffles are installed, checks that the resulting axial-to-tangential velocity ratio is acceptable, and estimates the surface vortex depth. It is intended for pitched-blade turbines operating in the transitional/turbulent regime inside cylindrical, flat-bottomed, fully baffled tanks.

Methodology & Formulas

  1. Unit conversion
    Dynamic viscosity: \( \mu \,[\mathrm{Pa\,s}] = \mu_{\text{cP}} \times 10^{-3} \)
    Kinematic viscosity: \( \nu \,[\mathrm{m^2\,s^{-1}}] = \nu_{\text{cSt}} \times 10^{-6} \)
    Rotational speed: \( N \,[\mathrm{rps}] = N_{\text{rpm}} / 60 \)
  2. Reynolds number
    \[ Re = \frac{\rho N D^2}{\mu} \]
    Flow regimeRe range
    Laminar< 10
    Transitional10 – 10,000
    Turbulent> 10,000
  3. Baffle width rule
    ConditionBaffle width / Tank diameter
    \( Re > 10,000 \)0.08
    \( Re \le 10,000 \)0.05
  4. Maximum tangential velocity (solid-body)
    \[ V_{\theta,\max} = \pi N D \]
  5. Baffle reduction factor
    Number of bafflesResidual factor \( f \)
    40.15
    60.06
    other0.15 (fallback)
    Residual tangential velocity: \( V_{\theta} = f \cdot V_{\theta,\max} \)
  6. Flow number and pumping capacity
    For a pitched-blade turbine the flow number is taken as \( N_Q = 0.55 \).
    Volumetric flow rate: \( Q = N_Q N D^3 \)
  7. Average axial velocity
    Tank cross-section: \( A = \pi T^2 / 4 \)
    Axial velocity: \( V_z = Q / A \)
  8. Velocity ratio
    \[ \frac{V_{\theta}}{V_z} \] Ratios ≫ 1 indicate swirl-dominated flow; values ≪ 1 imply good axial turnover.
  9. Empirical vortex depth (baffled tanks)
    \[ z_{\text{vortex}} = 0.01 \left( \frac{N_{\text{rpm}}}{100} \right) \left( \frac{D}{0.1\,\mathrm{m}} \right) \left( 1 - 0.8 \frac{N_b}{6} \right) \cdot \mathrm{m} \] The correlation is capped at 40% of the liquid height to avoid unphysical predictions.