Proceedings ArticleDOI
Shock-Boundary Layer Interaction Control using Innovative Micro-Vortex Generators in Supersonic Intake
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The article was published on 2017-06-02. It has received 1 citations till now. The article focuses on the topics: Shock (mechanics) & Supersonic speed.read more
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Book ChapterDOI
Near-Field Effectiveness of the Sub-Boundary Layer Vortex Generators Deployed in a Supersonic Intake
TL;DR: In this article, an attempt is made to control the interactions at the shock impact point in a Mach 2.2 mixed compression intake using micro-vortex generators (MVGs).
References
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Journal ArticleDOI
Shock wave/turbulent boundary layer interaction and its control
TL;DR: In this paper, a review of the fundamental properties of the interaction between a shock wave and a boundary layer is presented, with emphasis on the physics of phenomena involved in this process.
Journal ArticleDOI
Microramp Control of Supersonic Oblique Shock-Wave/Boundary-Layer Interactions
TL;DR: In this paper, the potential of microramp sub-boundary-layer vortex generators for flow control in supersonic engine inlets is investigated, focusing on the ability of these devices to beneficially affect oblique shockwave/ boundary-layer interactions.
Proceedings ArticleDOI
Optimal Control of Shock Wave Turbulent Boundary Layer Interactions Using Micro-Array Actuation
TL;DR: In this paper, the authors demonstrate the viability and economy of Response Surface Methodology (RSM) to determine optimal designs of micro-array actuation for controlling the shock wave turbulent boundary layer interactions within supersonic inlets and compare these concepts to conventional bleed performance.
Journal ArticleDOI
Effect of Microvortex Generators On Seperated Normal Shock/ Boundary Layer Interactions
HA Holden,Holger Babinsky +1 more
TL;DR: In this article, the effect of vortex generators placed upstream of a normal shock/turbulent boundary layer interaction at a Mach number of 1.5 and a freestream Reynolds number of 28 x 10 6 was investigated.
BookDOI
Drag Reduction by Shock and Boundary Layer Control
TL;DR: The EUROSHOCK II project as mentioned in this paper has been used for simulation of airfoil and wing flow with and without the use of shock wave and boundary layer interaction for the prediction of turbulent and unsteady transonic flows.