The compressible hybrid RANS/LES formulation using an additive operator

被引:40
|
作者
Sanchez-Rocha, Martin [1 ]
Menon, Suresh [1 ]
机构
[1] Georgia Inst Technol, Sch Aerosp Engn, Atlanta, GA 30332 USA
关键词
Hybrid RANS/LES approach; Hybrid RANS/LES governing equations; Near-wall modeling; Turbulent boundary layer; LES; AVERAGED NAVIER-STOKES; DETACHED-EDDY SIMULATION; LES-RANS; TURBULENT FLUCTUATIONS; INFLOW CONDITIONS; HEAT-TRANSFER; CHANNEL; MODELS; FLOW; INTERFACE;
D O I
10.1016/j.jcp.2008.11.021
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
In this work, the compressible governing equations for the hybrid Reynolds-averaged/large-eddy simulations are formally derived by applying a hybrid filter to the Navier-Stokes equations. This filter is constructed by linearly combining the Reynolds-average (RANS) and large-eddy simulation (LES) operators with a continuous blending function. The derived hybrid equations include additional terms that represent the interactions between RANS and LES formulations. The relevance of these terms is investigated in flat-plate turbulent boundary layer simulations and indicate that these additional terms play a fundamental role in compensating for the turbulence that is neither modeled nor resolved in the transition region between RANS and LES. Results also show that when the additional terms are included, the calculations are not very sensitive to the blending function implemented in the hybrid filter. In the contrary, when these terms are neglected and a step function is implemented in the hybrid filter, nonphysical discontinuities are predicted in the flow statistics. (C) 2008 Elsevier Inc. All rights reserved.
引用
收藏
页码:2037 / 2062
页数:26
相关论文
共 50 条
  • [21] Hybrid LES/RANS simulation of supersonic combustion using flamelet model
    Fan, Zhou-Qin
    Sun, Ming-Bo
    Liu, Wei-Dong
    Tuijin Jishu/Journal of Propulsion Technology, 2011, 32 (02): : 191 - 196
  • [22] A formulation for near-wall RANS/LES coupling
    Medic, Gorazd
    Templeton, Jeremy A.
    Kalitzin, Georgi
    INTERNATIONAL JOURNAL OF ENGINEERING SCIENCE, 2006, 44 (17) : 1099 - 1112
  • [23] RANS and hybrid LES/RANS simulations of flow over a square cylinder
    Ke, Jianghua
    ADVANCES IN AERODYNAMICS, 2019, 1 (01)
  • [24] LES AND HYBRID RANS/LES OF A FUNDAMENTAL TRAILING EDGE SLOT
    Lvanova, Elizaveta
    Laskowski, Gregory M.
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2014, VOL 5B, 2014,
  • [25] RANS and hybrid LES/RANS simulations of flow over a square cylinder
    Jianghua Ke
    Advances in Aerodynamics, 1
  • [26] Heat Transfer and Flow Structures for Structured Surfaces using LES and Hybrid RANS/LES Approach
    Turnow, J.
    Kornev, N.
    TURBULENCE HEAT AND MASS TRANSFER 9 (THMT-18), 2018, : 617 - 624
  • [27] Hybrid RANS/LES for active flow control
    Wang, Wei
    Siouris, Spiridon
    Qin, Ning
    AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2014, 86 (03): : 179 - 187
  • [28] Interface conditions for hybrid RANS/LES calculations
    Keating, A
    De Prisco, G
    Piomelli, U
    Balaras, E
    ENGINEERING TURBULENCE MODELLING AND EXPERIMENTS 6, 2005, : 349 - 358
  • [29] Active model split hybrid RANS/LES
    Haering, Sigfried W.
    Oliver, Todd A.
    Moser, Robert D.
    PHYSICAL REVIEW FLUIDS, 2022, 7 (01)
  • [30] Hybrid LES - RANS of complex geometry jets
    Eastwood, Simon J.
    Tucker, Paul G.
    INTERNATIONAL JOURNAL OF AEROACOUSTICS, 2011, 10 (5-6) : 659 - 684