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A Nonlinear Dynamic Subscale Model for Partially Resolved Numerical Simulation (PRNS)/Very Large Eddy Simulation (VLES) of Internal Non-Reacting FlowsA brief introduction of the temporal filter based partially resolved numerical simulation/very large eddy simulation approach (PRNS/VLES) and its distinct features are presented. A nonlinear dynamic subscale model and its advantages over the linear subscale eddy viscosity model are described. In addition, a guideline for conducting a PRNS/VLES simulation is provided. Results are presented for three turbulent internal flows. The first one is the turbulent pipe flow at low and high Reynolds numbers to illustrate the basic features of PRNS/VLES; the second one is the swirling turbulent flow in a LM6000 single injector to further demonstrate the differences in the calculated flow fields resulting from the nonlinear model versus the pure eddy viscosity model; the third one is a more complex turbulent flow generated in a single-element lean direct injection (LDI) combustor, the calculated result has demonstrated that the current PRNS/VLES approach is capable of capturing the dynamically important, unsteady turbulent structures while using a relatively coarse grid.
Document ID
20100022151
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Shih, Tsan-Hsing
(Ohio Aerospace Inst. Brook Park, OH, United States)
Liu, nan-Suey
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
May 1, 2010
Subject Category
Aeronautics (General)
Report/Patent Number
NASA/TM-2010-216323
E-17257
Report Number: NASA/TM-2010-216323
Report Number: E-17257
Funding Number(s)
WBS: WBS 561581.02.08.03.16.02
Distribution Limits
Public
Copyright
Public Use Permitted.
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