A flow simulation Methodology (FSM) is presented for computing the time-dependent behavior of complex compressible turbulent flows. The development of FSM was initiated in close collaboration with C. Speziale (then at Boston University). The objective of FSM is to provide the proper amount of turbulence modeling for the unresolved scales while directly computing the largest scales. The strategy is implemented by using state-of-the-art turbulence models (as developed for Reynolds averaged Navier-Stokes (RANS)) and scaling of the model terms with a “contribution function.” The contribution function is dependent on the local and instantaneous “physical” resolution in the computation. This physical resolution is determined during the actual simulation by comparing the size of the smallest relevant scales to the local grid size used in the computation. The contribution function is designed such that it provides no modeling if the computation is locally well resolved so that it approaches direct numerical simulations (DNS) in the fine-grid limit and such that it provides modeling of all scales in the coarse-grid limit and thus approaches a RANS calculation. In between these resolution limits, the contribution function adjusts the necessary modeling for the unresolved scales while the larger (resolved) scales are computed as in large eddy simulation (LES). However, FSM is distinctly different from LES in that it allows for a consistent transition between RANS, LES, and DNS within the same simulation depending on the local flow behavior and “physical” resolution. As a consequence, FSM should require considerably fewer grid points for a given calculation than would be necessary for a LES. This conjecture is substantiated by employing FSM to calculate the flow over a backward-facing step and a plane wake behind a bluff body, both at low Mach number, and supersonic axisymmetric wakes. These examples were chosen such that they expose, on the one hand, the inherent difficulties of simulating (physically) complex flows, and, on the other hand, demonstrate the potential of the FSM approach for simulations of turbulent compressible flows for complex geometries.

1.
Smagorinsky
,
J.
, 1963, “
General Circulation Experiments With the Primitive Equations. I. The Basic Experiment
,”
Mon. Weather Rev.
0027-0644,
91
, pp.
99
164
.
2.
Spalart
,
P. R.
, 2000, “
Strategies for Turbulence Modelling and Simulations
,”
Int. J. Heat Fluid Flow
0142-727X,
21
, pp.
252
263
.
3.
Boris
,
J.
,
Grinstein
,
F.
,
Oran
,
E.
, and
Kolbe
,
R.
, 2000, “
New Insights Into Large Eddy Simulation
,”
Fluid Dyn. Res.
0169-5983,
10
(
4–6
), pp.
199
228
.
4.
Fureby
,
C.
, and
Grinstein
,
F.
, 1999, “
Monotonically Integrated Large Eddy Simulation of Free Shear Flows
,”
AIAA J.
0001-1452,
37
(
5
), pp.
544
556
.
5.
Speziale
,
C. G.
, and
Fasel
,
H. F.
, 1993, Office of Naval Research: Accelerated Research Initiative for Complex Turbulent Flows, Washington D.C., Program Monitor: L. Patrick Purtell.
6.
Speziale
,
C. G.
, 1996, “
Computing Non-Equilibrium Turbulent Flows With Time-Dependent RANS and VLES
,”
15th International Conference on Numerical Methods in Fluid Dynamics
, June 24–28,
Monterey, CA
.
7.
Speziale
,
C. G.
, 1998, “
Turbulence Modeling for Time-Dependent RANS and VLES: A Review
,”
AIAA J.
0001-1452,
36
(
2
), pp.
173
184
.
8.
Fasel
,
H. F.
,
Seidel
,
J.
, and
Wernz
,
S.
, 2002, “
A Methodology for Simulation of Complex Turbulent Flows
,”
J. Fluids Eng.
0098-2202,
124
, pp.
933
942
.
9.
Speziale
,
C. G.
, 1998, “
A Combined Large-Eddy Simulation and Time-Dependent RANS Capability for High-Speed Compressible Flows
,”
J. Sci. Comput.
0885-7474,
13
(
3
), pp.
253
274
.
10.
Pope
,
S. B.
, 2000,
Turbulent Flows
,
Cambridge University Press
,
Cambridge
.
11.
Batten
,
P.
,
Goldberg
,
U.
, and
Chakravarthy
,
S.
, 2000, “
Sub-Grid Turbulence Modelling for Unsteady Flow With Acoustic Resonance
,” AIAA Report No. 2000-0473.
12.
Gatski
,
T. B.
, and
Speziale
,
C. G.
, 1993, “
On Explicit Algebraic Stress Models for Complex Turbulent Flows
,”
J. Fluid Mech.
0022-1120,
254
, pp.
59
78
.
13.
Rumsey
,
C. L.
,
Gatski
,
T. B.
, and
Morrison
,
J. H.
, 2000, “
Turbulence Model Predictions of Strongly Curved Flow in a U-Duct
,”
AIAA J.
0001-1452,
38
(
8
), pp.
1394
1402
.
14.
Durbin
,
P. A.
, 1993, “
A Reynolds Stress Model for Near Wall Turbulence
,”
J. Fluid Mech.
0022-1120,
249
, pp.
465
498
.
15.
Sarkar
,
S.
, 1992, “
The Pressure-Dilatation Correlation in Compressible Flows
,”
Phys. Fluids A
0899-8213,
4
(
12
), pp.
2674
2682
.
16.
von Terzi
,
D. A.
, 2004, “
Numerical Investigation of Transitional and Turbulent Backward-Facing Step Flows
,” Ph.D. thesis, University of Arizona.
17.
Sandberg
,
R. D.
, 2004, “
Numerical Investigation of Transitional and Turbulent Supersonic Axisymmetric Wakes
,” Ph.D. thesis, University of Arizona.
18.
Henderson
,
R. D.
, 1997, “
Nonlinear Dynamics and Pattern Formation in Turbulent Wake Transition
,”
J. Fluid Mech.
0022-1120,
352
, pp.
65
112
.
19.
Williamson
,
C. H. K.
, 1996, “
Vortex Dynamics in the Cylinder Wake
,”
Annu. Rev. Fluid Mech.
0066-4189,
28
, pp.
477
539
.
You do not currently have access to this content.