Add to ORKGThe present study attempts to identify the eigenmodes that are associated with the screech mechanism by means of Dynamic Mode Decomposition (DMD) and a method based on the Arnoldi eigenvalue algorithm, respectively
This paper explores the screech closure mechanism for different axisymmetric modes in shock-containi...
Screech tones are produced by imperfectly expanded jets under certain conditions. This paper provide...
A linear stability analysis method, employing a linearized flow solver combined with the Arnoldi alg...
The present study attempts to identify the eigenmodes that are associated with the screech mechanism...
Supersonic jet noise has been an important research topic for decades, both for its relevance within...
The dynamics of a supersonic jet emanating from a high-aspect-ratio rectangular nozzle is investigat...
The paper employs STFT (Short Time Fourier Transform) to extract and analyze the noise components of...
The applicability of two different eigenvalue algorithms coupled with an axisymmetric RANS solver to...
The screech tone of an underexpanded jet is numerically calculated without any specific modeling for...
We study and model the resonance mechanism underlying the generation of A1 and A2 screech modes in a...
The fairly recent methodology, the so called Dynamic Mode Decomposition, is investigated for the Aft...
Design and analysis methods for gas turbine combustors or afterburners need to be improved in partic...
In this paper, a detailed time evolution analysis is presented for the interaction between the insta...
Predicting thermo-acoustic instabilities in combustion chambers remains an important issue. These in...
Operating a convergent-divergent nozzle under overexpanded conditions can lead to supersonic flow se...
This paper explores the screech closure mechanism for different axisymmetric modes in shock-containi...
Screech tones are produced by imperfectly expanded jets under certain conditions. This paper provide...
A linear stability analysis method, employing a linearized flow solver combined with the Arnoldi alg...
The present study attempts to identify the eigenmodes that are associated with the screech mechanism...
Supersonic jet noise has been an important research topic for decades, both for its relevance within...
The dynamics of a supersonic jet emanating from a high-aspect-ratio rectangular nozzle is investigat...
The paper employs STFT (Short Time Fourier Transform) to extract and analyze the noise components of...
The applicability of two different eigenvalue algorithms coupled with an axisymmetric RANS solver to...
The screech tone of an underexpanded jet is numerically calculated without any specific modeling for...
We study and model the resonance mechanism underlying the generation of A1 and A2 screech modes in a...
The fairly recent methodology, the so called Dynamic Mode Decomposition, is investigated for the Aft...
Design and analysis methods for gas turbine combustors or afterburners need to be improved in partic...
In this paper, a detailed time evolution analysis is presented for the interaction between the insta...
Predicting thermo-acoustic instabilities in combustion chambers remains an important issue. These in...
Operating a convergent-divergent nozzle under overexpanded conditions can lead to supersonic flow se...
This paper explores the screech closure mechanism for different axisymmetric modes in shock-containi...
Screech tones are produced by imperfectly expanded jets under certain conditions. This paper provide...
A linear stability analysis method, employing a linearized flow solver combined with the Arnoldi alg...