In Part I a wave packet model is used to show that a time-developing mixing layer produces a Mach wave pattern similar to the one produced by a spatial-developing mixing layer. However, this kind of similarity does not exist for the sound emitted by subsonic sound sources. A method to analyse temporal direct numerical simulation (DNS) results for the Mach wave pattern is then developed and demonstrated using numerical results of the wave-packet model. The method is applied to the temporal DNS results of a supersonic mixing layer undergoing transition to turbulence. Two dominant Mach waves are revealed. The first wave originates from about the time of the Λ-vortex structure dominance in the layer. The second wave appears just prior to the fi...
Mach wave radiation from supersonic jets is revisited to better quantify the extent to which lineari...
AbstractThe far-field noise radiated from mixing layers is determined by the near-field flow dynamic...
International audienceAcoustic radiation of shock free supersonic jets is modified in comparison wit...
In Part II a large-scale sound source in a time-developing planar free mixing layer is studied using...
Mach number and thermal effects on the mechanisms of sound generation and propagation are investigat...
The sound generated by vortex pairing in a two-dimensional compressible mixing layer is investigated...
The sound field created by wave packets has been subject to rigorous experimental, analytical and nu...
AbstractIn practical situations, natural transition determines the transition to turbulence process....
Dans ce travail, une méthodologie numérique a été développée afin d obtenir avec précision le calcul...
A numerical code solving acoustic analogies to predict shock-induced noise is developed. Both Lighth...
The effect of Mach number on the evolution of instabilities in the compressible mixing layer is inve...
Sound from a mixing layer flow is computed directly by solving the Navier-Stokes equations on a comp...
Non-linear sound propagation is investigated computationally by simulating compressible time-develop...
Direct numerical simulations of turbulent shear flows and their radiated acoustic fields have provid...
The radiation of sound from artificial sources in a developing shear layer is studied numerically, i...
Mach wave radiation from supersonic jets is revisited to better quantify the extent to which lineari...
AbstractThe far-field noise radiated from mixing layers is determined by the near-field flow dynamic...
International audienceAcoustic radiation of shock free supersonic jets is modified in comparison wit...
In Part II a large-scale sound source in a time-developing planar free mixing layer is studied using...
Mach number and thermal effects on the mechanisms of sound generation and propagation are investigat...
The sound generated by vortex pairing in a two-dimensional compressible mixing layer is investigated...
The sound field created by wave packets has been subject to rigorous experimental, analytical and nu...
AbstractIn practical situations, natural transition determines the transition to turbulence process....
Dans ce travail, une méthodologie numérique a été développée afin d obtenir avec précision le calcul...
A numerical code solving acoustic analogies to predict shock-induced noise is developed. Both Lighth...
The effect of Mach number on the evolution of instabilities in the compressible mixing layer is inve...
Sound from a mixing layer flow is computed directly by solving the Navier-Stokes equations on a comp...
Non-linear sound propagation is investigated computationally by simulating compressible time-develop...
Direct numerical simulations of turbulent shear flows and their radiated acoustic fields have provid...
The radiation of sound from artificial sources in a developing shear layer is studied numerically, i...
Mach wave radiation from supersonic jets is revisited to better quantify the extent to which lineari...
AbstractThe far-field noise radiated from mixing layers is determined by the near-field flow dynamic...
International audienceAcoustic radiation of shock free supersonic jets is modified in comparison wit...