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Supersonic Cavity Flow Feedback Mechanism by czar6023.24 is a document available to read on EtoBox.

This document presents a study on the feedback-loop mechanism in supersonic open cavity flows using large-eddy simulation (LES). The research investigates the causality between feedback acoustic waves and shedding vortices, identifying the generation mechanism of these waves through phase-averaged analysis and Proper Orthogonal Decomposition (POD). The findings contribute to understanding the complex interactions in high-speed cavity flows, which have significant implications for aerospace engineering appli

Author

czar6023.24

Language

EN