Flow visualization for separation vortex around airfoil

نویسندگان
چکیده

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

Flow Visualization Around a Non - Circular Tube

The flow behavior around a cam shaped tube in cross flow has been investigated experimentally using flow visualization and pressure distribution measurement. The range of attack angle and Reynolds number based on an equivalent circular diameter are within 0 ≤ α ≤ 360˚ and 2 x 104 < Reeq < 3.4 x 104, respectively. The pressure drag features are clarified in relation to the flow behavior around t...

متن کامل

Instabilities of Stationary Inviscid Compressible Flow around an Airfoil

In this paper we numerically solve the stationary inviscid flow around an airfoil. Using the second-order explicit Runge–Kutta method in combination with the MUSCL scheme and the minmod limiter, we do not obtain a machine accurate solution. This has already been observed in literature and is explained by the non-differentiability of the minmod limiter. An analysis of the limiter shows that it i...

متن کامل

High Reynolds Viscous Flow Simulation Past the Elliptical Airfoil by Random Vortex Blob

In this paper, numerical simulation for a two-dimensional viscous and incompressible flow past the elliptical airfoil is presented by Random Vortex Blob (RVB). RVB is a numerical technique to solve the incompressible, two-dimensional and unsteady Navier-Stocks equations by converting them to rotational non-primitive formulations. In this method, the velocity vector at a certain point can be cal...

متن کامل

Active Control of Flow Separation Over an Airfoil

Designing an aircraft without conventional control surfaces is of interest to aerospace community. In this direction, smart actuator devices such as synthetic jets have been proposed to provide aircraft maneuverability instead of control surfaces. In this article, a numerical study is performed to investigate the effects of unsteady suction and blowing oil airfoils. The unsteady suction and blo...

متن کامل

Flow Physics of Separated Flow over a Naca 0015 Airfoil and Detection of Flow Separation

J. P. Bonnet, W. L. Siauw, L. Cordier, J. Tensi Laboratoire d’Etudes Aérodynamiques, UMR CNRS 6609, ENSMA, Téléport 2, 1 Av. Clément Ader, BP 40109, 86961 Futuroscope Chasseneuil Cedex, France Bernd R. Noack Berlin Institute of Technology MB1 Straße des 17. Juni 135, D-10623 Berlin, Germany L. N. Cattafesta III Interdisciplinary Microsystems Group, University of Florida, Gainesville, FL, USA 32611

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: Journal of the Visualization Society of Japan

سال: 1998

ISSN: 1884-037X,0916-4731

DOI: 10.3154/jvs.18.supplement1_155