The evolution of hydrodynamic instability modes self-excited by harmonically related natural screech tones was experimentally investigated. A convergent rectangular nozzle with an aspect ratio of 9.63 was used to produce a supersonic shock containing jet. Measurements in the flow-field were made using standard hot-film probes positioned only in the subsonic (outer) portions of the flow. The hydrodynamic instability mode observed in the shear layer at the screech frequency was observed to be antisymmetric (sinuous) about the smaller dimension of the jet, whereas its harmonic was observed to be symmetric (varicose). In addition, the near-field noise measurements indicated that the radiated screech tone noise was out of phase on either side of...
Under certain conditions, shock-containing jets produce an intense tone referred to as screech. Scre...
International audienceExperimental evidence is provided to demonstrate that the upstream-travelling ...
The topics covered include the following: the three components of supersonic jet noise; shock cell s...
It is known experimentally that an imperfectly expanded rectangular jet from a thin-lip convergent n...
The generation mechanism of screech harmonics in supersonic exhausts is revealed using shadowgraph i...
International audienceThe generation of screech tones in an underexpanded jet is investigated by mea...
Many supersonic military aircraft and some of the modern civilian aircraft (such as the Boeing 777) ...
In significantly underexpanded jets, screech inherently ceases to exist. This paper studies screech ...
Understanding screech is especially important for the design of advanced aircraft because screech ca...
The influence of shear layer excitation on the mixing of supersonic rectangular jets was studied exp...
An analytical model is developed to study the sound produced by the interaction between shock and in...
An imperfectly expanded supersonic jet, invariably, radiates both broadband noise and discrete frequ...
A temporally-developing supersonic round jet at a Mach number of 2 and at a diameter-based Reynolds ...
The paper employs STFT (Short Time Fourier Transform) to extract and analyze the noise components of...
International audienceWe study and model the resonance mechanism underlying the generation of A1 and...
Under certain conditions, shock-containing jets produce an intense tone referred to as screech. Scre...
International audienceExperimental evidence is provided to demonstrate that the upstream-travelling ...
The topics covered include the following: the three components of supersonic jet noise; shock cell s...
It is known experimentally that an imperfectly expanded rectangular jet from a thin-lip convergent n...
The generation mechanism of screech harmonics in supersonic exhausts is revealed using shadowgraph i...
International audienceThe generation of screech tones in an underexpanded jet is investigated by mea...
Many supersonic military aircraft and some of the modern civilian aircraft (such as the Boeing 777) ...
In significantly underexpanded jets, screech inherently ceases to exist. This paper studies screech ...
Understanding screech is especially important for the design of advanced aircraft because screech ca...
The influence of shear layer excitation on the mixing of supersonic rectangular jets was studied exp...
An analytical model is developed to study the sound produced by the interaction between shock and in...
An imperfectly expanded supersonic jet, invariably, radiates both broadband noise and discrete frequ...
A temporally-developing supersonic round jet at a Mach number of 2 and at a diameter-based Reynolds ...
The paper employs STFT (Short Time Fourier Transform) to extract and analyze the noise components of...
International audienceWe study and model the resonance mechanism underlying the generation of A1 and...
Under certain conditions, shock-containing jets produce an intense tone referred to as screech. Scre...
International audienceExperimental evidence is provided to demonstrate that the upstream-travelling ...
The topics covered include the following: the three components of supersonic jet noise; shock cell s...