kth_logo.gif

Article

Design and tests of wind-tunnel sidewalls for receptivity experiments on a swept wing

Authors: Romano, D.G., Alfredsson, P.H., Hanifi, A., Örlü, R., Tillmark, N.T., Borodulin, V. I., Ivanov, A. V., Kachanov, Y.S., Minervino, M.
Document Type: Book
Pubstate: Published
Journal: Applied Mechanics and Materials
Volume: 390   96-102
Year: 2013

Abstract

This document explains in its first part the design procedure adopted to design the contoured sidewalls of a swept-wing airfoil section mounted in a wind tunnel in order to satisfy the infinite swept-wing approximation. In the second part, the experimental set-up is described as well as the first results of the experimental campaign. The sidewalls are shown to play their role properly and satisfactorily provide the infinite swept-wing conditions required for subsequent investigations of the most important vortex receptivity mechanisms responsible for excitation of crossflow and Tollmien-Schlichting instability modes in the airfoil boundary layer.

http://dx.doi.org/10.4028/www.scientific.net/AMM.390.96