Studies of turbulent boundary layer flow through direct numerical simulation

نویسنده

  • Martin Skote
چکیده

The objective has been to study turbulent boundary layers under adverse pressure gradients (APG) through direct numerical simulation (DNS). The numerical code is based on a pseudo-spectral technique which is suitable for the simple geometry (flat plate) considered here. A large effort has been put into the optimization of the numerical code on various super computers. Five large simulations have been performed, ranging from a zero pressure gradient boundary layer to a separating flow. The simulations have revealed many features of APG turbulent boundary layers which are difficult to capture in experiments. Especially the near-wall behavior has been investigated thoroughly, both through the statistical and instantaneous flow. Theoretical work based on the turbulent boundary layer equation has been conducted with the aim to develop near-wall laws suitable for turbulence models. The conditions for self-similarity and relations between mean flow parameters have been reviewed and applied in the DNS. The results from the simulations have confirmed the theoretical part of this work. The turbulent flows have also been investigated using turbulence models. A boundary layer under strong APG is difficult to predict correctly, and the separating boundary layer is one of the most difficult flows in this respect. The near-wall damping was improved by comparing DNS data and model predictions. The asymptotic behavior of an APG boundary layer for large Reynolds numbers has been determined through asymptotic analysis and with the aid of turbulence models. The DNS data have also been utilized for the investigation of instantaneous turbulence structures. The turbulent boundary layer was found to be populated by near-wall low-speed streaks and vortices shaped like a horseshoe, in agreement with earlier investigations. The instability mechanism behind the formation of these vortices is examined through a simulation of an artificial low-speed streak introduced in a laminar boundary layer. The turbulence statistics from the simulations have also been compared with other simulations of turbulent boundary layers and Couette flow. Descriptors: Turbulence, direct numerical simulation, boundary layer, separation, parallel computers, turbulence modelling.

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

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

Large-eddy simulation of turbulent flow over an array of wall-mounted cubes submerged in an emulated atmospheric boundary-layer

Turbulent flow over an array of wall-mounted cubic obstacles has been numerically investigated using large-eddy simulation. The simulations have been performed using high-performance computations with local cluster systems. The array of cubes are fully submerged in a simulated deep rough-wall atmospheric boundary-layer with high turbulence intensity characteristics of environmental turbulent fl...

متن کامل

Direct numerical simulation of separating turbulent boundary layers

Direct numerical simulation of two turbulent boundary layer flows has been performed. The boundary layers are both subject to a strong adverse pressure gradient. In one case a separation bubble is created while in the other the boundary layer is everywhere attached. The data from the simulations are used to investigate scaling laws near the wall, a crucial concept in turbulence models. Theoreti...

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

Direct numerical simulation of hypersonic turbulent boundary layers. Part 1. Initialization and comparison with experiments

A systematic procedure for initializing supersonic and hypersonic turbulent boundary layers at controlled Mach number and Reynolds number conditions is described. The initialization is done by locally transforming a true direct numerical simulation flow field, and results in a nearly realistic initial magnitude of turbulent fluctuations, turbulence structure and energy distribution. The time sc...

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 2001