A general computational approach is presented for numerical modeling o
f viscous flow in baffled, impeller-stirred-tank reactors. A multibloc
k, body-fitted grid structure facilitates modeling of various impeller
and baffle designs, and a new procedure offers averaged velocity data
from a complex 3-D CFD dataset. Impellers are modeled precisely, elim
inating the need for inputting experimental velocity data for boundary
conditions. The method can be used quickly to obtain extremely detail
ed flow computations at a fraction of the cost of computing unsteady m
oving grid solutions. A steady-state computational approach that negle
cts the relative motion between impeller and baffles yields numerical
results comparably accurate to full unsteady computations for laminar
flow at a fraction of the time and expense. The approximate steady-sta
te method is used to predict power requirements of a Rushton turbine i
n laminar flow. An unsteady, moving grid technique provides time-accur
ate solutions for the pow inside an impeller-stirred reactor with side
-wall baffles. These computed results are compared with those using th
e approximate steady-state method and with experimental measurements.
The unsteady, moving gild method uses two different initial conditions
: one starting from rest and the other starting from an approximate st
eady-state solution obtained at the starting position of the impeller
relative to rite baffles. For unsteady simulations of laminar flow in
stirred vessels, the final operating condition call be achieved much m
ore efficiently if the solution obtained from the steady-state procedu
re is used as an approximate initial condition.