Feature-based analysis of a turbulent boundary layer under spanwise wall oscillation

نویسندگان

چکیده

Spanwise wall oscillations alter the organization of low-speed streaks and ejections in turbulent boundary layers, eventually leading to skin friction drag reduction. Such flow regimes are represented by pointwise statistics or spatial correlation. This work attempts quantify systematic distortions dominant structures feature-analysis, intended overcome dispersion observed correlation functions. Furthermore, data from tomographic particle image velocimetry employed clarify mechanism that inhibits hairpin auto-generation, as described Kempaiah et al. [“3-dimensional based evaluation skin-friction reduction spanwise oscillation,” Phys. Fluids 32(8), 085111 (2020)]. Based on instantaneous distribution Reynolds stresses, a specific template is defined for ejections. Events corresponding this collected parametrized with their occurrence, geometrical properties (length orientation), dynamics (intensity). The approach compared most practiced statistical analysis explain significance features extracted detection algorithm relation mechanism. Data comparing stationary oscillating drag-reducing regime (A + osc = 100, T 100) investigated near-wall region (y < 100). Ejections systematically exhibit positive pitch, supporting hypothesis only rear region, close wall, affected motion. A side-tilt elongated ejection events past phase maximum oscillation velocity, which hypothesized inhibit auto-generation. latter indicates dependence regime. results also indicate reduced approximately 10% 15%, respectively, further consolidating rapid lateral distortion being responsible different organizations region.

برای دانلود باید عضویت طلایی داشته باشید

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

Direct Numerical Simulation of Supersonic Turbulent Boundary Layer with Spanwise Wall Oscillation

Weidan Ni 1,†, Lipeng Lu 1,†, Catherine Le Ribault 2,† and Jian Fang 1,3,*,† 1 National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, School of Energy and Power Engineering, Beihang University, 37 Xueyuan Road, Haidian District, Beijing 100191, China; [email protected] (W.N.); [email protected] (L.L.) 2 Laboratoire de Mécanique Des Fluides (LMFA), Ecole Centrale...

متن کامل

Turbulent Drag Reduction by Spanwise Wall Oscillations

The objective of this paper is to examine the effectiveness of wall oscillation as a control scheme of drag reduction. Two flow configurations are considered: constant flow rate and constant mean pressure gradient. The Navier-Stokes equations are solved using Fourier-Chebyshev spectral methods and the oscillation in sinusoidal form is enforced on the walls through boundary conditions for the sp...

متن کامل

Turbulent Drag Reduction by Spanwise Wall Oscillations

The objective of this paper is to examine the effectiveness of wall oscillation as a control scheme of drag reduction. Two flow configurations are considered: constant flow rate and constant mean pressure gradient. The Navier-Stokes equations are solved using Fourier-Chebyshev spectral methods and the oscillation in sinusoidal form is enforced on the walls through boundary conditions for the sp...

متن کامل

DNS of turbulent boundary layer with time-periodic blowing through a spanwise slot

Direct numerical simulations are extended to see the effects of time-periodic blowing frequency from a spanwise slot on a turbulent boundary layer. The time-periodic blowing frequency is given in a range 0≤f≤0.08 at a fixed blowing amplitude of A=0.5. The effects of the blowing frequency are scrutinized by examining the phaseor time-averaged turbulent statistics. A most effective blowing freque...

متن کامل

Measurements of streamwise and spanwise fluctuating velocity components in a high Reynolds number turbulent boundary layer

Measurements of the streamwise and spanwise fluctuating velocity components are obtained in a high Reynolds number turbulent boundary layer using custom made sub-miniature hot wires. These measurements are made over a range of Reynolds numbers from Reτ ≈ 3,000 to Reτ ≈ 10,500, but at fixed unit Reynolds number U∞/ν (Reτ = δUτ/ν; where ν is the kinematic viscosity, Uτ is the friction velocity an...

متن کامل

ذخیره در منابع من


  با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید

ژورنال

عنوان ژورنال: Physics of Fluids

سال: 2022

ISSN: ['1527-2435', '1089-7666', '1070-6631']

DOI: https://doi.org/10.1063/5.0127220