The fairly recent methodology, the so called Dynamic Mode Decomposition, is investigated for the Afterburner test case in order to see if the methodology is able to capture thermo-acoustic instabilities. Previous papers deal with the prediction of such instabilities using the Arnoldi extraction technique. The present paper compares these two approaches in order to see their advantages and drawbacks regarding the present case of study. The linearized solver chosen in the Arnoldi extraction technique is based on the Linearized Navier Stokes Equations (LNSE). As a main concern of the study, the structures and frequencies of the buzz (~ 120 Hz) and the screech modes (~ 1200 Hz) are compared using both methodologies. Additional cases are also st...
The prediction of combustion instabilities is crucial for aircraft engines manufacturers to ensure t...
One-dimensional methods used for solving acoustic instabilities are of doubtful value in the design ...
The excitation of acoustic oscillations in combustion chambers is well-known as an unwelcome phenome...
Design and analysis methods for gas turbine combustors or afterburners need to be improved in partic...
Predicting thermo-acoustic instabilities in combustionchambers remains an important issue. These ins...
Design and analysis methods for gas turbine combustors or afterburners have to be improved in partic...
A previously developed eigenmode extraction algorithm, based on a time-domain linearized flow solver...
In numerous industrial systems, acoustic resonances are synonymous with loud noise and dramatic stru...
Combustor or afterburner instabilities such as buzz and screech modes can lead to major damage in ga...
The dynamic mode decomposition (DMD) is applied to a 3-dimensional chamber in order to identify acou...
The thesis presents the author s research on numerical methods for Com-putational Aeroacoustics and ...
Strong ow eld instabilities associated with acoustic resonance have been observed in many engineerin...
The dynamics of a supersonic jet emanating from a high-aspect-ratio rectangular nozzle is investigat...
Supersonic jet noise has been an important research topic for decades, both for its relevance within...
The article describes the features of numerical simulation of acoustic oscillation excitation in the...
The prediction of combustion instabilities is crucial for aircraft engines manufacturers to ensure t...
One-dimensional methods used for solving acoustic instabilities are of doubtful value in the design ...
The excitation of acoustic oscillations in combustion chambers is well-known as an unwelcome phenome...
Design and analysis methods for gas turbine combustors or afterburners need to be improved in partic...
Predicting thermo-acoustic instabilities in combustionchambers remains an important issue. These ins...
Design and analysis methods for gas turbine combustors or afterburners have to be improved in partic...
A previously developed eigenmode extraction algorithm, based on a time-domain linearized flow solver...
In numerous industrial systems, acoustic resonances are synonymous with loud noise and dramatic stru...
Combustor or afterburner instabilities such as buzz and screech modes can lead to major damage in ga...
The dynamic mode decomposition (DMD) is applied to a 3-dimensional chamber in order to identify acou...
The thesis presents the author s research on numerical methods for Com-putational Aeroacoustics and ...
Strong ow eld instabilities associated with acoustic resonance have been observed in many engineerin...
The dynamics of a supersonic jet emanating from a high-aspect-ratio rectangular nozzle is investigat...
Supersonic jet noise has been an important research topic for decades, both for its relevance within...
The article describes the features of numerical simulation of acoustic oscillation excitation in the...
The prediction of combustion instabilities is crucial for aircraft engines manufacturers to ensure t...
One-dimensional methods used for solving acoustic instabilities are of doubtful value in the design ...
The excitation of acoustic oscillations in combustion chambers is well-known as an unwelcome phenome...