Control of bypass transitional flow past an aerofoil by plasma actuation
IR@NAL: CSIR-National Aerospace Laboratories, Bangalore
View Archive Info| Field | Value | |
| Title |
Control of bypass transitional flow past an aerofoil by plasma actuation
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| Creator |
Sengupta, TK
Suman, VK Bhumkar, YG |
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| Subject |
Aeronautics (General)
Fluid Mechanics and Thermodynamics |
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| Description |
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.
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| Publisher |
Multi-Science Publishing Co.,
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| Date |
2012
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| Type |
Journal Article
PeerReviewed |
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| Format |
application/pdf
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| Identifier |
http://nal-ir.nal.res.in/11924/1/fulltext.pdf
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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| Relation |
http://dx.doi.org/10.1260/1756-8315.3.2-3.117
http://nal-ir.nal.res.in/11924/ |
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