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Parametric studies of aerofoil-vortex interaction; a numerical approach using LES

Published online by Cambridge University Press:  27 January 2016

M. Ilie ,
F. Nitzsche  and
E. Matida
M. Ilie*
Affiliation:
University of Central Florida, Orlando, Florida, USA
F. Nitzsche
Affiliation:
Carleton University, Ottawa, Canada
E. Matida
Affiliation:
Carleton University, Ottawa, Canada
*
marcel.Ilie@ucf.edu
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Abstract

The influence of angle-of-attack and vortex-aerofoil vertical miss-distance on the aerofoil-vortex mechanism of interaction is investigated numerically using the large-eddy simulation approach. The study concerns the aerofoil-vortex interaction (AVI) phenomena encountered in the rotorcraft aerodynamics. The studies are performed for a Reynolds number of 1·3 × 106 based on the chord (c = 0·2m) of the aerofoil and free-stream velocity U = 100ms−1. The studies are conducted for three different angles-of-attack (α = 0°, and α = 5°, α = 10°) and vertical miss-distances (h = 0·0m, h = −0·01, h = −0·02m) respectively. The present study shows that the magnitude of lift coefficient and flow separation, at the instant of interaction, decay with the increase of angle-of-attack and vertical miss-distance.

Type
Research Article
Information
The Aeronautical Journal , Volume 115 , Issue 1173 , November 2011 , pp. 703 - 711
Copyright
Copyright © Royal Aeronautical Society 2011 

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