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.
| Original language | English |
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| Title of host publication | Aeronautical Journal|Aeronaut J |
| Pages | 597-602 |
| Number of pages | 5 |
| Volume | 105 |
| Publication status | Published - 2001 |
| Event | CEAS Aerospace Aerodynamics Research Conference, London - Duration: 1 Jan 1824 → … |
Conference
| Conference | CEAS Aerospace Aerodynamics Research Conference, London |
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| Period | 1/01/24 → … |