A numerical method is presented that allows large eddy simulation (LES) of
turbulent Rows in complex geometric configurations with moving boundaries a
nd that retains the advantages of solving the Navier-Stokes equations on fi
xed orthogonal grids. The boundary conditions are applied independently of
the grid by assigning body forces over surfaces that need not coincide with
coordinate lines. The use of orthogonal, nondeforming grids simplifies gri
d generation, facilitates the implementation of high-order, nondissipative
discretization schemes, and minimizes the spatial and temporal variations i
n filter width that complicate unstructured deforming-grid LES, Dynamic sub
grid-scale turbulence models are particularly appealing in combination with
the body-force procedure because the dynamic model accounts automatically
for the presence of solid walls without requiring damping functions. The me
thod is validated by simulations of the turbulent Row in a motored axisymme
tric piston-cylinder assembly for which detailed experimental measurements
are available. Computed mean and rms velocity profiles show very good agree
ment with measured ensemble averages. The present numerical code runs on sm
all, personal computerlike workstations. For a comparable level of accuracy
, computational requirements (memory and CPU time) are at least a factor of
10 lower compared to published simulations for the same configuration obta
ined using an unstructured, boundary-fitted deforming-grid approach.