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Author

Nadaraja Pillai

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Sep 2026

Hybrid flow control method for supersonic jet noise suppression: a Mach number effect

This study examines the noise reduction potential of the proposed hybrid flow control nozzle for designs with Mach numbers 1.4 and 1.8. The Schlieren image indicates that jets exiting the hybrid flow control nozzle (DS-CHN) exhibit two notable changes: a reduction in the dimensions of the supersonic core jet and an i...

Manikandan Kabaleeshwaran, R. Das, Nadaraja Pillai · 0 citations

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