Abstract
Large eddy simulation (LES) of combustion problems involve highly nonlinear terms that, when filtered, result in a contribution from subgrid (subfilter) fluctuations of the scalar, Z, to the filtered value. The subgrid contribution requires modeling. In the approximate reconstruction using moments (ARM) method, a surrogate scalar field is obtained from the available filtered field by approximate reconstruction, a purely mathematical procedure, as well as additional physics-based information required to match specific scalar moments, in the simplest case, the subgrid variance. Here, we present results from a priori and a posteriori studies of the ARM model in the case of a spatially evolving plane jet. The nonlinearities considered are of two types: a polynomial function and an exponential function. A priori analysis, using data from direct numerical simulation (DNS), is carried out using different filter sizes. One of these filter sizes is chosen to perform a LES and obtain a posteriori results with a dynamic eddy diffusivity model. The a priori tests show that the ARM model is able to capture the subgrid part of the variance accurately over a wide range of filter sizes and reasonable well for higher polynomials up to an eighth power as well as the exponential nonlinearity. The a posteriori case shows good behavior of the subgrid model, similar to that in the a priori test.
Original language | English (US) |
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State | Published - 2002 |
Event | 40th AIAA Aerospace Sciences Meeting and Exhibit 2002 - Reno, NV, United States Duration: Jan 14 2002 → Jan 17 2002 |
Other
Other | 40th AIAA Aerospace Sciences Meeting and Exhibit 2002 |
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Country/Territory | United States |
City | Reno, NV |
Period | 1/14/02 → 1/17/02 |
ASJC Scopus subject areas
- Space and Planetary Science
- Aerospace Engineering