Affiliation:
1. Department of Aerospace Engineering, Texas A&M University, College Station, TX 77843
Abstract
A turbulence bridging method purported for any filter-width or scale resolution—fully averaged to completely resolved—is developed. The method is given the name partially averaged Navier-Stokes (PANS) method. In PANS, the model filter width (extent of partial averaging) is controlled through two parameters: the unresolved-to-total ratios of kinetic energy (fk) and dissipation (fε). The PANS closure model is derived formally from the Reynolds-averaged Navier-Stokes (RANS) model equations by addressing the following question: if RANS represents the closure for fully averaged statistics, what is the corresponding closure for partially averaged statistics? The PANS equations vary smoothly from RANS equations to Navier-Stokes (direct numerical simulation) equations, depending on the values of the filter-width control parameters. Preliminary results are very encouraging.
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics
Reference17 articles.
1. Speziale, C. G.
, 1996, “Computing Non-Equilibrium Flows With Time-Dependent RANS and VLES,” 15th ICNMFD.
2. Spalart, P. R.
, 2000, “Trends in Turbulence Treatments,” Fluids 2000, Denver, AIAA Paper No. 2000-2306.
3. Batten, P., Goldberg, U., and Chakravarthy, S., 2002, “LNS-An Approach Towards Embedded LES,” AIAA Paper No. 2002-0427.
4. Time-Accurate Simulations and Acoustic Analysis of Slat Free Shear Layer;Khorrami;AIAA J.
5. Khorrami, M. R., Singer, B., and Lockard, D., 2002, “Time-Accurate Simulations and Acoustic Analysis of Slat Free Shear Layer: Part 2,” AIAA/CEAS Aeroacoustics Conference and Exhibit, Breckenridge, CO, AIAA Paper No. 2002-2579.
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