Tomographic-PIV investigation of the 3D Separation behaviour of a micro-ramp controlled SWBLI

Conference Paper (2017)
Author(s)

Kapileswar Nayak (TU Delft - Structural Integrity & Composites)

RHM Giepman

Ferry F.J. Schrijer (TU Delft - Aerodynamics)

Bas Van Oudheusden (TU Delft - Aerodynamics)

Research Group
Aerodynamics
Copyright
© 2017 K. Nayak, R.H.M. Giepman, F.F.J. Schrijer, B.W. van Oudheusden
More Info
expand_more
Publication Year
2017
Language
English
Copyright
© 2017 K. Nayak, R.H.M. Giepman, F.F.J. Schrijer, B.W. van Oudheusden
Research Group
Aerodynamics
Reuse Rights

Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.

Abstract

Micro-ramp vortex generators (or micro-ramps) have gained popularity as promising alternatives to boundary layer bleed for high speed flow-control applications. Micro-ramps generate a counter-rotating vortex pair which leads to a more separation resistant boundary layer. Furthermore, they modulate the size of the shock induced separation bubble along the span such that individual cells of three-dimensional separation are formed.
In the current study, the highly three-dimensional nature of such a micro-ramp controlled SWBLI is visualized by using tomographic-PIV. The 3D mean flow field of the interaction is presented, while the 3D separation behaviour is further characterized by the separation probability of the interaction Psep at different wall-parallel planes. The largest reduction in Psep occurs along the micro-ramp centreline where separation is basically eliminated. Additionally, it is found that the total volume of separation is decreased by 70% when compared to an uncontrolled SWBLI.

Files

3AF_S01B_S_NAYAK_P.pdf
(pdf | 1.52 Mb)
License info not available