Predicting transition with wall-distance-free SST k-ω model

被引:8
|
作者
Rahman, M. M. [1 ]
机构
[1] Hangzhou Dianzi Univ, Sch Mech Engn, Hangzhou 310018, Peoples R China
关键词
Flow transition; LRN turbulent flow; Transitional WDF SST model; gamma-Re-theta model; Airfoil; ARTIFICIAL COMPRESSIBILITY METHOD; DIRECT NUMERICAL-SIMULATION; REYNOLDS-STRESS; FLOW; SEPARATION; TURBULENCE; AIRFOILS; LAYER;
D O I
10.1016/j.compfluid.2022.105704
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
Unlike the correlation-based gamma-Re-theta transition model, an exceptionally simplified approach is applied to extend the wall-distance-free (WDF) model toward transition predictions. An anisotropic stress-intensity parameter as a function of eddy-to-laminar viscosity ratio is introduced, preserving the "flow-structure-adaptive" characteristic. The prospective parameter is included with the constitutive relation for the eddy-viscosity. The proposed formulation is intrinsically plausible, having a dramatic influence on the prediction of bypass, separation-induced and natural transitions. The newly devised transitional WDF (TWDF) model is further modified to compute separation-induced transition over a low-Reynolds number (LRN) airfoil. The curiosity toward airfoil performance at an LRN has been executed with growing attention to marine autonomous systems. An extra viscous-production term P-K(lim) is added to the turbulent kinetic energy (k) certain proper development of k at the viscous sublayer region. Reliance on this P-K(lim) is likely to be suitable for forecasting separation-induced transition over an LRN airfoil. Results illustrate that the TWDF model sustains decent agreement with the four-equation gamma-Re-theta transition model.
引用
收藏
页数:13
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