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2 articles for “Micro Vortex Generator”
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Control of Separation Induced on the Wing of Transonic Speed Aircraft by Means of Micro Vortex Generator
Abstract: Normal 0 false false false EN-US X-NONE X-NONE MicrosoftInternetExplorer4 This experimental study provides an assessment of the potential of applying a control device to mitigate undesired separation formed on the wing of an aircraft causing instability of the airliner. They are used in a wide range of aircrafts and yet needs to be improved for wider applications.The study was conducted in a transonic wind tunnel. The concept of passive control, …
Published in Journal of Aerospace Engineering & Technology · Vol. 1, Issue 2, 2011 Read article
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Review of Shock-Boundary Layer Controlled Interactions Studies in High Speed Intakes
Abstract: Normal 0 false false false EN-US X-NONE X-NONE The present work review about the studies conducted by various researchers on shock-boundary layer interactions and their control in high speed intakes. The shock-boundary layer interactions have been a topic of immense interest among the researchers for past many decades due to their associated aerodynamic and aerothermodynamic phenomena. The sudden retardation at the shock impact point promotes, either the boundary layer thickening …
Published in Journal of Aerospace Engineering & Technology · Vol. 5, Issue 3, 2015 · pp. 1–14 Read article