Sub-Filter-Scale Shear Stress Deficit in Hypersonic Wall-Bounded Turbulence and Its Implications for Large-Eddy Simulation
Speaker: Takahiko Toki, Purdue University
Presentation
Seminar Slide Deck (PDF-8.3MB)
Abstract
Turbulent boundary layers on hypersonic vehicles entail significant skin-friction and heat-transfer loads. Accurate prediction of the boundary-layer state is therefore of paramount importance for the design of efficient thermal protection systems. While Reynolds–averaged Navier–Stokes (RANS) simulations are widely used in engineering applications due to their relatively low computational cost, mid- to high-fidelity approaches such as large-eddy simulation (LES) are required to capture the dynamics of turbulent fluctuations. However, current LES models often exhibit strong grid dependence in the prediction of skin friction and heat transfer, highlighting the need for a better understanding of near-wall behavior in hypersonic wall-bounded turbulence.
In this talk, the limitations of current LES models are first illustrated through simulations of hypersonic conical boundary layers. The focus then shifts to sub-filter-scale (SFS) turbulent behavior, investigated using direct numerical simulations (DNS) of hypersonic Couette flow with particular attention to shear-stress components. Semi-local scaling laws are shown to collapse mean profiles and second-order turbulence statistics despite strong wall-normal gradients of temperature and density. In contrast, the SFS shear stress exhibits an unexpected profile characterized by a region of pronounced stress deficit. The underlying mechanism of this deficit is elucidated through instantaneous flow visualization and statistical quadrant analysis, providing insight into near-wall turbulence dynamics in hypersonic flows.
Biography