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Effect of Micro Vortex Generator Width on Vortex Characteristics
AIAA AVIATION 2022 Forum, 2022Abhishek Khare, Shashank Khurana
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EFFECT OF MICRO-VORTEX GENERATOR GEOMETRY ON SEPARATION CHARACTERISTICS OF SUPERSONIC INLET
Ballistics 2025Shock boundary layer interaction (SBLI) for supersonic inlet can cause flow separation which can lead to increased drag, unstart conditions resulting in reduction in performance and efficiency. One of the important techniques of SBLI mitigation is use of micro-vortex generator (MVG) located upstream of the shock impingement in order to control the flow
Rahul Chopde +2 more
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Application of Micro-Vortex Generators for Turbulent Flow Separation Control
1999Flow separation on multi-element high-lift airfoils can be a complicated function of geometry and flight conditions, and can not be predicted reliably at this time. Previous reports have shown that certain high-lift configurations exhibit boundary-layer separation on the flap at low angles of attack, while fully attached flap flow occurs near ...
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Supersonic Jet Noise Reduction Using Micro Vortex Generators
AIAA AVIATION 2021 FORUM, 2021Junhui Liu +4 more
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Numerical Study of Drag Reduction by Conventional and Micro Vortex Generators
AIAA AVIATION 2021 FORUM, 2021Sandeep E. James +2 more
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Effectiveness of micro-vortex generators in tandem in high-speed flows
AIAA AVIATION 2020 FORUM, 2020Shilpa Sajeev +3 more
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Effects of vortex generator on subcooled flow boiling characteristics in micro-channel
International Journal of Heat and Mass Transfer, 2023Dawei Zhuang, Guoliang Ding
exaly
Impact of Micro Vortex Generators on aerodynamic performance
AIAA SCITECH 2025 ForumAlessandro Argiuolo +4 more
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