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.
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A Methodology for Simulating Compressible Turbulent Flows
Hermann F. Fasel,
Hermann F. Fasel
Department of Aerospace and Mechanical Engineering,
e-mail: faselh@email.arizona.edu
The University of Arizona
, Tucson, Arizona, 85721
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Dominic A. von Terzi,
Dominic A. von Terzi
Department of Aerospace and Mechanical Engineering,
e-mail: dominic@email.arizona.edu
The University of Arizona
, Tucson, Arizona, 85721
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Richard D. Sandberg
Richard D. Sandberg
Department of Aerospace and Mechanical Engineering,
e-mail: richard@email.arizona.edu
The University of Arizona
, Tucson, Arizona, 85721
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Hermann F. Fasel
Department of Aerospace and Mechanical Engineering,
The University of Arizona
, Tucson, Arizona, 85721e-mail: faselh@email.arizona.edu
Dominic A. von Terzi
Department of Aerospace and Mechanical Engineering,
The University of Arizona
, Tucson, Arizona, 85721e-mail: dominic@email.arizona.edu
Richard D. Sandberg
Department of Aerospace and Mechanical Engineering,
The University of Arizona
, Tucson, Arizona, 85721e-mail: richard@email.arizona.edu
J. Appl. Mech. May 2006, 73(3): 405-412 (8 pages)
Published Online: September 30, 2005
Article history
Received:
January 15, 2004
Revised:
September 30, 2005
Citation
Fasel, H. F., von Terzi, D. A., and Sandberg, R. D. (September 30, 2005). "A Methodology for Simulating Compressible Turbulent Flows." ASME. J. Appl. Mech. May 2006; 73(3): 405–412. https://doi.org/10.1115/1.2150231
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