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Visualisation of flow separation with shear-sensitive liquid crystals

Published online by Cambridge University Press:  04 July 2016

S. O’Brien  and
S. Zhong
S. O’Brien
Affiliation:
School of Engineering, University of Manchester, Manchester, UK
S. Zhong
Affiliation:
School of Engineering, University of Manchester, Manchester, UK
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Abstract

Coatings of chiral-nematic liquid crystals are known to change colour under different levels of surface shear stress. In this study, the liquid crystal coating was used to provide information about flow separation and reattachment on a backward facing step and a delta wing respectively. The tests were carried out at a free-stream velocity of 25ms-1. The Reynolds number based on the step height of the backward facing step is 16,000 and based on the chord length of the delta wing is 270,000. The study revealed that the locations of boundary-layer separation and reattachment can be identified from spatial variations in the surface colour. Agreement was obtained between the results acquired from liquid crystal and surface oil flow technique. The variation in hue was used to improve the determination on the location of flow characteristics. This study showed that the liquid crystal coating is an effective method for the qualitative study of separated flow characteristics.

Type
Research Article
Information
The Aeronautical Journal , Volume 105 , Issue 1052 , October 2001 , pp. 597 - 602
Copyright
Copyright © Royal Aeronautical Society 2001 

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