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Analysis of Passive Panel Flutter Control using Micro-Ramp
AIAA SCITECH 2022 Forum, 2022Seshendra Palakurthy +4 more
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Micro Ramps in Supersonic Turbulent Boundary Layers: An experimental and numerical study
2014The micro vortex generator (MVG) is used extensively in low speed aerodynamic problems and is now extended into the supersonic flow regime to solve undesired flow features that are associated with shock wave boundary layer interactions (SWBLI) such as flow separation and associated unsteadiness of the interaction system.
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Understanding Micro-Ramp Control of Supersonic Shock Wave Boundary Layer Interactions
2007Abstract : This research investigated the potential of micro-ramp sub-boundary layer vortex generators for flow control of oblique shock boundary layer interactions (SBLIs) which is relevant to supersonic engine inlets. These novel devices can delay shock-induced separation and improve boundary layer health, thus offering the potential to reduce the ...
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Tomographic-PIV investigation of the 3D Separation behaviour of a micro-ramp controlled SWBLI
2017Aerodynamics
Nayak, K. (author) +3 more
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