Effects of confinement, impinging shock deflection angle, and Mach number on the flow field of a supersonic open cavity
Sreejita Bhaduri, Mohammed Ibrahim Sugarno, Ashoke De

TL;DR
This study investigates how confinement, shock deflection, and Mach number influence the flow dynamics and oscillation frequencies of a supersonic open cavity using advanced numerical simulations.
Contribution
It provides new insights into the effects of confinement and flow conditions on cavity oscillations through detailed 3D simulations and frequency analysis.
Findings
Confinement increases oscillation frequency.
Higher deflection angles induce Kelvin-Helmholtz instability.
Increasing Mach number intensifies flow instability.
Abstract
Cavities exhibit inherent self-sustaining oscillations driven by the coupling between their hydrodynamic and acoustic properties. In practical applications, cavities are often placed within confinements that introduce compression waves, significantly influencing their primary flow characteristics. The oscillations in cavities have widespread applications, such as in fuel-air mixing, heat exchangers, and landing gears However, when resonance occurs, these oscillations can lead to structural failures. Therefore, understanding cavity oscillations under diverse geometrical configurations and flow conditions is essential. The present study examines the impact of top wall confinement on an open cavity with a length-to-depth ratio (L/D) ratio of 3 at Mach 1.71, along with the effects of varying deflection angles on flow characteristics and the influence of an increased Mach number on…
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