This article provides a comprehensive overview of noise prediction and mitigation
methodologies within the context of rocket launch events. The first section presents noise …

Heated transitional supersonic jets exhausting from a rectangular nozzle at over-expanded
conditions are investigated by Large Eddy Simulations and Ffowcs-Williams and Hawkings …

The present study proposed the framework of the spatiotemporal superresolution
measurement based on the sparse regression with dimensionality reduction using the …

The flow and acoustic fields of jets at a Mach number of 3.1 im**ing on a plate at 15 D of
the jet nozzle exit, where D is the nozzle diameter, have been investigated using highly …

In this paper, the Pseudo shock structure in a convergent–long divergent duct is investigated
using large eddy simulation on the basis of Smagorinsky–Lilly,​ Wall-Adapting Local Eddy …

The Reynolds number effect on the aeroacoustic fields of a supersonic jet was
experimentally investigated via particle image velocimetry (PIV), schlieren visualization, and …

Three-dimensional density fields of the twin jets were numerically and experimentally
investigated. The present study focused on the comparison of the density distribution for the …

The surface pressure field generated by a supersonic im**ing jet on a vertical flat plate
was measured using a pressure-sensitive paint (PSP) and a double-pulsed laser. The Mach …

The exact dynamic mode decomposition (DMD) was applied to the nonsequential image
dataset obtained by the double-pulsed schlieren measurement of a supersonic im**ing …

Data assimilation using particle image velocimetry (PIV) and Reynolds-averaged Navier–
Stokes (RANS) simulation was performed for an ideally expanded supersonic jet flying at a …