Président du jury : Patrick Huerre (Ecole Polytechnique)The basic purpose of the present thesis is to examine the phenomenon ofacoustic radiation of supersonic jet flows by resorting to the linearinstability theory.Thus, the downstream development of vortical structures is represented asa collection of spatially growing instability waves of various frequencies.At the local level description, it is shown that a simple topologicalrelationship between roots of the dispersion relation and branch cutsdetermines two generic configurations for the time-asymptotic Green's function,depending on control parameters.Both configurations leads to the conclusion that a local analysis is notappropriate to describe the sound emission.In some cases, the cros...
Motivated by the problem of jet–flap interaction noise, we study the tonal dynamics that occurs when...
The objective of this thesis is twofold: firstly, to study the dynamics inherent in the near field o...
This work aims to study the dynamics of and noise generated by large-scale structures in a Mach 0.9 ...
Cette thèse est consacrée a l étude du rayonnement acoustique des jets supersoniques, dans le cadre ...
La thèse est relative à la compréhension de la physique et au contrôle des émissions acoustiques dan...
Self-sustaining sounds related to aero-acoustic coupling occurs in impinging jets when a feedback lo...
Cette étude s'inscrit dans l'effort de réduction des nuisances sonores des avions au décollage. Une ...
Dans le but de réduire le bruit de jet, source principale de nuisance sonore au décollage d'un avion...
An initial value problem with relevance to jet noise is investigated. A plane parallel jet flow is s...
Broadband shock-associated noise is an important component of the overall noise generated by modern ...
Increasingly stringent aircraft noise regulations require the development of innovative noise reduct...
An analytical model is developed to study the sound produced by the interaction between shock and in...
The generation of discrete acoustic tones in the compressible flow around an aerofoil is addressed i...
In this thesis, we study the formation of coherent structures in the early stages of transition from...
Linear stability theory has been intensively used over the past decades for the characterization of ...
Motivated by the problem of jet–flap interaction noise, we study the tonal dynamics that occurs when...
The objective of this thesis is twofold: firstly, to study the dynamics inherent in the near field o...
This work aims to study the dynamics of and noise generated by large-scale structures in a Mach 0.9 ...
Cette thèse est consacrée a l étude du rayonnement acoustique des jets supersoniques, dans le cadre ...
La thèse est relative à la compréhension de la physique et au contrôle des émissions acoustiques dan...
Self-sustaining sounds related to aero-acoustic coupling occurs in impinging jets when a feedback lo...
Cette étude s'inscrit dans l'effort de réduction des nuisances sonores des avions au décollage. Une ...
Dans le but de réduire le bruit de jet, source principale de nuisance sonore au décollage d'un avion...
An initial value problem with relevance to jet noise is investigated. A plane parallel jet flow is s...
Broadband shock-associated noise is an important component of the overall noise generated by modern ...
Increasingly stringent aircraft noise regulations require the development of innovative noise reduct...
An analytical model is developed to study the sound produced by the interaction between shock and in...
The generation of discrete acoustic tones in the compressible flow around an aerofoil is addressed i...
In this thesis, we study the formation of coherent structures in the early stages of transition from...
Linear stability theory has been intensively used over the past decades for the characterization of ...
Motivated by the problem of jet–flap interaction noise, we study the tonal dynamics that occurs when...
The objective of this thesis is twofold: firstly, to study the dynamics inherent in the near field o...
This work aims to study the dynamics of and noise generated by large-scale structures in a Mach 0.9 ...