An analytical technique for the calculation of linear decay coefficients in combustors with acoustic absorbers is presented. Tuned circumferential slot acoustic absorbers were designed for the first three transverse modes of oscillation, and decay coefficients for these absorbers were found as a function of backing distance for seven different chamber configurations. The effectiveness of the absorbers for off-design values of the combustion response and acoustic mode is also investigated. Results indicate that for tuned absorbers the decay coefficient increases approximately as the cube of the backing distance. For most off-design situations the absorber still provides a damping effect. However, if an absorber designed for some higher mode ...
Stabilizing influence of acoustic cavities on acoustic modes of combustion instability in rocket eng...
Combustion chambers are naturally prone to acoustic instabilities that originate from flame propagat...
The article of record as published may be found at http://dx.doi.org/10.1121/1.2144006Since 1930, th...
Nonarray absorbing devices were investigated for use in rocket thrust chambers as instability suppre...
The acoustic resonance spectrum and the dissipation of speci¦c modes in combustors equipped with abs...
The acoustic resonance spectrum and the dissipation of specific modes in combustors equipped with ab...
The acoustic resonance spectrum and the dissipation of specific modes in combustors equipped with ab...
Mechanical absorption of acoustic oscillations in simulated rocket combustion chamber
An analytical technique for the evaluation of combustion stability in rocket motors with partial len...
Analytical and computational techniques were developed to predict the stability behavior of liquid p...
International audienceThe coupled acoustic system of a cylindrical combustor and an absorber cavity ...
Combustion instability is recognized as one of the major problems frequently faced by engineers duri...
The development is discussed of analytical techniques and numerical methods for the prediction of th...
Combustion instabilities in rocket engines are caused by coupling between the combustion processes a...
Helmholtz resonators with variable cavity depths tested with unstable rocket combusto
Stabilizing influence of acoustic cavities on acoustic modes of combustion instability in rocket eng...
Combustion chambers are naturally prone to acoustic instabilities that originate from flame propagat...
The article of record as published may be found at http://dx.doi.org/10.1121/1.2144006Since 1930, th...
Nonarray absorbing devices were investigated for use in rocket thrust chambers as instability suppre...
The acoustic resonance spectrum and the dissipation of speci¦c modes in combustors equipped with abs...
The acoustic resonance spectrum and the dissipation of specific modes in combustors equipped with ab...
The acoustic resonance spectrum and the dissipation of specific modes in combustors equipped with ab...
Mechanical absorption of acoustic oscillations in simulated rocket combustion chamber
An analytical technique for the evaluation of combustion stability in rocket motors with partial len...
Analytical and computational techniques were developed to predict the stability behavior of liquid p...
International audienceThe coupled acoustic system of a cylindrical combustor and an absorber cavity ...
Combustion instability is recognized as one of the major problems frequently faced by engineers duri...
The development is discussed of analytical techniques and numerical methods for the prediction of th...
Combustion instabilities in rocket engines are caused by coupling between the combustion processes a...
Helmholtz resonators with variable cavity depths tested with unstable rocket combusto
Stabilizing influence of acoustic cavities on acoustic modes of combustion instability in rocket eng...
Combustion chambers are naturally prone to acoustic instabilities that originate from flame propagat...
The article of record as published may be found at http://dx.doi.org/10.1121/1.2144006Since 1930, th...