International audienceThe interactions between upstream-propagating guided jet waves and shear-layer instability waves near the nozzle of subsonic and nearly ideally expanded supersonic, isothermal free jets are investigated for jets at Mach numbers between 0.50 and 2 with fully laminar exit boundary layers of different thicknesses. The velocity spectra in the shear layers downstream of the nozzle exhibit strong narrow peaks for the first azimuthal modes, associated with growing Kelvin-Helmholtz instability waves. The frequencies of the predominant peaks are close, but not necessarily equal, to those of the most amplified instability waves predicted from the mean flow fields using linear stability analysis. They also fall in most cases with...
Two cases are considered. The first is concerned with mean flows of the Blasius type wherein the ins...
Mach wave radiation from supersonic jets is revisited to better quantify the extent to which lineari...
The presence and properties of acoustic peaks near the nozzle of impinging rocket jets have been inv...
The purpose of this paper is to characterize and model waves that are observed within the potential ...
The purpose of this paper is to examine the generation and nature of the large coherent structures o...
The evolution of the large scale structures and the mean field were investigated in axisymmetric and...
International audienceThe characteristics of acoustic tones near the nozzle of jets are investigated...
International audienceThe influence of the nozzle-exit boundary-layer profile on high-subsonic jets ...
Non-modal instability analysis of the shear layer near the nozzle of a supersonic under-expanded imp...
The impingement of a round jet issued from a convergent nozzle is known to produce intense tonal noi...
Motivated by the problem of jet–flap interaction noise, we study the tonal dynamics that occurs when...
We perform an inviscid, spatial stability analysis of supersonic, heated round jets with the mean pr...
The stability of "top-hat" and fully developed jet profiles is investigated by an inviscid linear st...
Motivated by the problem of jet–flap interaction noise, we study the tonal dynamics that occurs when...
For many years investigations have been conducted to understand the flow instabilities that lead to ...
Two cases are considered. The first is concerned with mean flows of the Blasius type wherein the ins...
Mach wave radiation from supersonic jets is revisited to better quantify the extent to which lineari...
The presence and properties of acoustic peaks near the nozzle of impinging rocket jets have been inv...
The purpose of this paper is to characterize and model waves that are observed within the potential ...
The purpose of this paper is to examine the generation and nature of the large coherent structures o...
The evolution of the large scale structures and the mean field were investigated in axisymmetric and...
International audienceThe characteristics of acoustic tones near the nozzle of jets are investigated...
International audienceThe influence of the nozzle-exit boundary-layer profile on high-subsonic jets ...
Non-modal instability analysis of the shear layer near the nozzle of a supersonic under-expanded imp...
The impingement of a round jet issued from a convergent nozzle is known to produce intense tonal noi...
Motivated by the problem of jet–flap interaction noise, we study the tonal dynamics that occurs when...
We perform an inviscid, spatial stability analysis of supersonic, heated round jets with the mean pr...
The stability of "top-hat" and fully developed jet profiles is investigated by an inviscid linear st...
Motivated by the problem of jet–flap interaction noise, we study the tonal dynamics that occurs when...
For many years investigations have been conducted to understand the flow instabilities that lead to ...
Two cases are considered. The first is concerned with mean flows of the Blasius type wherein the ins...
Mach wave radiation from supersonic jets is revisited to better quantify the extent to which lineari...
The presence and properties of acoustic peaks near the nozzle of impinging rocket jets have been inv...