Spatial linear stability analysis is used to study the axisymmetric screech tones generated by
twin converging round nozzles at low supersonic Mach numbers. Vortex-sheet and finite …

View Video Presentation: https://doi. org/10.2514/6.2023-4488. vid A study of the different
waves involved in the screech resonance loop in rectangular jets is undertaken in this work …

The fixed-total-pressure-based air-blowing method in free-jet wind tunnels only produces
uniformity in a limited area for supersonic jets. To address the issue, we investigated the …

This article delves into the dynamics of inviscid annular supersonic jets, akin to those exiting
converging-diverging nozzles in over-expanded regimes. It focuses on the first azimuthal …

This paper investigates the aeroacoustic properties of dual-stream co-axial supersonic jets,
focusing on sound generation at the engine nozzle exit, which significantly contributes to …

This work presents an experimental investigation of the resonance generated by a subsonic
and supersonic jet issuing from a convergent nozzle and impinging on a flat plate normal to …

This paper presents an experimental study on the transient behaviors of droplet
approaching a solid surface driven by shock/blast waves. The experiments were conducted …

The investigation focuses on the propagation of a gas shock wave in a self-gravitating ideal
gas under the influence of a spatially diminishing azimuthal magnetic field. It is believed that …