Evolution of a Boundary Layer from Laminar Stagnation-Point Flow Towards Turbulent Separation

نویسنده

  • B. Scheichl
چکیده

We present the most relevant recent findings that allow for a rational timeaveraged description of laminar–turbulent transition of an incompressible nominally two-dimensional and steady boundary layer along the impermeable surface of a rigid blunt body. Rigorous application of matched asymptotic expansions for sufficiently high values of both the Reynolds number and a turbulence-level gauge parameter shows that the presence of a leading-edge stagnation point is associated with the generation of a turbulent shear layer that exhibits an asymptotically small streamwise velocity deficit. Remarkably, however, the turbulence intensity never reaches its theoretically possible maximum that conforms to fully developed turbulent flow. 1 Motivation and Problem Formulation Although desirable for engineering applications, a reliable prediction of the flow past a more-or-less bluff body for realistically high values of the globally formed Reynolds number, Re, is presently still unavailable, notwithstanding the undeniable ongoing progress of computational methods like Direct Numerical and Large-Eddy Simulation. That is, a self-consistent comprehensive description of the time-mean process of gross separation that is essentially derived from first principles in the limit Re → ∞ yet provides a challenging problem of theoretical hydrodynamics. As an interesting step forwards, here we focus on the asymptotic structure of the attached boundary layer (BL) evolving from the stagnation point, S, of the external flow. Let the natural coordinates x, y along and perpendicular to the (perfectly smooth) body surface with origin in S, the corresponding Reynolds-averaged velocity components u, v, and the Reynolds stresses be non-dimensional with respect to a typical half-diameter L of the obstacle, the speed U of the incident parallel free-stream Bernhard Scheichl · Alfred Kluwick Institute of Fluid Mechanics and Heat Transfer, Resselgasse 3/E322, A-1040 Vienna, Austria, e-mail: [email protected],[email protected]

برای دانلود رایگان 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

Numerical Simulation of Separation Bubble on Elliptic Cylinders Using Three-equation k-? Turbulence Model

Occurrence of laminar separation bubbles on solid walls of an elliptic cylinder has been simulated using a recently developed transitional model for boundary layer flows. Computational method is based on the solution of the Reynolds averaged Navier-Stokes (RANS) equations and the eddy-viscosity concept. Transitional model tries to simulate streamwise fluctuations, induced by freestream turbulen...

متن کامل

Stagnation-point flow of a viscous fluid towards a stretching surface with variable thickness and thermal ‎radiation‎

‎In the present analysis‎, ‎we study the boundary layer flow of an incompressible viscous fluid near the two-dimensional stagnation-point flow over a stretching surface‎. ‎The effects of variable thickness and radiation are also taken into account and assumed that the sheet is non-flat‎. ‎Using suitable transformations‎, ‎the governing partial differential equations are first converted to ordin...

متن کامل

تحلیل جریان خارجی با استفاده از تلفیق جریان لایه مرزی و جریان ایده آل

In this paper, the analysis of two dimensional viscous incompressible flow around bodies with multiple industrial applications, is presented. Both of boundary layer flow and potential flow have been analysed repeatedly and in this way, the major parameters of flow are calculated. Laminar and turbulent boundary layer flow are solved with the aid of an virtual flow normal to the surface of the bo...

متن کامل

The Effect of Square Splittered and Unsplittered Rods in Flat Plate Heat Transfer Enhancement

A square splittered and unsplittered rod is placed in a turbulent boundary layer developed over a flat plate. The effect of the resulting disturbances on the local heat transfer coefficient is then studied. In both cases the square rod modifies the flow structure inside the boundary layer. As a result, a stagnation point, a jet and wake area are generated around the square rod, each making a co...

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

عنوان ژورنال:

دوره   شماره 

صفحات  -

تاریخ انتشار 2009