Sengupta, TK and Suman, VK and Bhumkar, YG (2012) Control of bypass transitional flow past an aerofoil by plasma actuation. International Journal of Emerging Multidisciplinary Fluid Sciences, 3 (2-3). pp. 117-134. ISSN 1756-8315
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Abstract
In this work, we have studied effects of plasma actuation while controlling bypass transition of flow over the top surface of DU96-W-180 aerofoil. We have discussed some of the important plasma simulation models proposed in the literature and presented results using a hybrid model given by [Lemire and Vo, J. Turbomach., 2011, 133(1), 011017]. Results show that the computed body force is localized near the electrodes. Due to action of plasma generated body force, bypass transition on the aerofoil surface is delayed.
Item Type: | Article |
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Additional Information: | Copyright to this article belongs to M/s. Multi-Science Publishing Co., |
Uncontrolled Keywords: | Flow control;Plasma actuation;Direct numerical simulation; Bypass transition;Transition delay |
Subjects: | AERONAUTICS > Aeronautics (General) ENGINEERING > Fluid Mechanics and Thermodynamics |
Depositing User: | Ms. Alphones Mary |
Date Deposited: | 13 Feb 2014 04:52 |
Last Modified: | 13 Feb 2014 04:52 |
URI: | http://nal-ir.nal.res.in/id/eprint/11924 |
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