Vortex Dynamics in Transitional and Turbulent Boundary Layers

نویسنده

  • Peter S. Bernard
چکیده

The dynamics of transitional and turbulent boundary layers is explored via a hybrid vortex filament/finite volume simulation scheme in which vortical structures are identified without the constraints imposed by the traditional assumption that they are synonymous with rotational regions. Vortex furrows consisting of elongated, streamwise-oriented, raised perturbations to the wall vorticity layer overlying low-speed streaks are found to be the principal structural element appearing during the Klebanoff type transition. A number of dynamical properties of the furrows are considered here providing new insights into such questions as why both one and two-legged hairpins appear, why and how low-speed streaks form and why they persist, why hairpin-like rotational regions form, and why mushroom-like shapes and “pockets” are found in smoke visualizations of boundary layers. Consideration of the relationship between vortex furrows and the complex vortical structures appearing within the fully turbulent zone provides some insights into why turbulence in the boundary layer is self-sustaining.

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

ثبت نام

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

Transitional-turbulent spots and turbulent-turbulent spots in boundary layers.

Two observations drawn from a thoroughly validated direct numerical simulation of the canonical spatially developing, zero-pressure gradient, smooth, flat-plate boundary layer are presented here. The first is that, for bypass transition in the narrow sense defined herein, we found that the transitional-turbulent spot inception mechanism is analogous to the secondary instability of boundary-laye...

متن کامل

Hairpin Vortex Formation a Case Study for Unsteady Visualization

To better understand the vortex dynamics of coherent structures in turbulent and transitional bound ary layers we consider direct numerical simulation of the interaction between a at plate boundary layer ow and an isolated hemispherical roughness element Of principal interest is the evolution of hairpin vortices that form an interlacing pattern in the wake of the hemisphere lift away from the w...

متن کامل

Boundary layer transition in high-speed flows due to roughness

Direct numerical simulation (DNS) is used to study the effect of individual (hemispherical) and distributed roughness on supersonic flat plate boundary layers. In both cases, roughness generates a shear layer and counter–rotating pairs of unsteady streamwise vortices. The vortices perturb the shear layer, resulting in trains of hairpin vortices and a highly unsteady flow. Mach 3.37 flow past a ...

متن کامل

Enhanced Visualization of Late-stage Transitional Structures Using Vortex Identiication and Automatic Feature Extraction

The unsteady Navier{Stokes equations ooer a large variety of instantaneous solutions even for rather simple boundary conditions once the relevant spatial and temporal scales of the problem at hand are adequately resolved. This is especially true for DNS (Direct Numerical Simulation) of laminar-turbulent transition, where an initially lam-inar ow, disturbed by some unsteady uctuations \breaks do...

متن کامل

Aerodynamic Noise Computation of the Flow Field around NACA 0012 Airfoil Using Large Eddy Simulation and Acoustic Analogy

The current study presents the results of the aerodynamic noise prediction of the flow field around a NACA 0012 airfoil at a chord-based Reynolds number of 100,000 and at 8.4 degree angle of attack. An incompressible Large Eddy Simulation (LES) turbulence model is applied to obtain the instantaneous turbulent flow field. The noise prediction is performed by the Ffowcs Williams and Hawkings (FW-...

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

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

ثبت نام

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

عنوان ژورنال:

دوره   شماره 

صفحات  -

تاریخ انتشار 2011