In this paper, we present experimental observations and phenomenological modeling of the intermittent dynamics that emerge while mitigating thermoacoustic instability by rotating the otherwise static swirler in a lean premixed, laboratory-scale combustor. Starting with a self-excited thermoacoustically unstable combustor, here we find that a progressive increase in swirler rotation rate does not uniformly decrease amplitudes of coherent, sinusoidal pressure or heat-release-rate oscillations. Instead, these oscillations emerge as high-amplitude bursts separated by low-amplitude noise in the signal. At increased rotational speeds, the high-amplitude coherent oscillations become scarce and their duration in the signal reduces. The velocity fie...
Self-exited thermoacoustic instability is undesirable in gas turbines and other propulsion systems ...
This thesis was awarded the Leonardo da Vinci prize in 2013 for outstanding doctoral research in flu...
Thermoacoustic instability in a lean premixed combustor is a major impediment towards reliable opera...
In this paper, we present a novel initial attempt on analysis of the mitigation mechanism of instabi...
Open-loop control is known to be an effective strategy for controlling self-excited thermoacoustic o...
The dynamic transition from combustion noise to combustion instability was investigated experimental...
Thermoacoustic systems with a turbulent reactive flow, prevalent in the fields of power and propulsi...
In the context of this work we attempt to examine the intermittency characteristics of thermoacousti...
We investigate the onset of thermoacoustic instabilities in a turbulent combustor terminated with an...
An experimental study on a turbulent, swirl-stabilized backward facing step combustor is conducted t...
A detailed study concerning a novel, dynamic control strategy for mitigating thermoacoustic instabil...
A joint experimental and computational study of thermoacoustic instabilities in a model swirl-stabil...
The thermoacoustic coupling caused by dynamic flow/flame interactions was investigated in a gas-turb...
Turbulent premixed flames often experience thermoacoustic instabilities when the combustion heat rel...
This experimental study focuses on characterizing the nonlinear combustion dynamics prior to blowout...
Self-exited thermoacoustic instability is undesirable in gas turbines and other propulsion systems ...
This thesis was awarded the Leonardo da Vinci prize in 2013 for outstanding doctoral research in flu...
Thermoacoustic instability in a lean premixed combustor is a major impediment towards reliable opera...
In this paper, we present a novel initial attempt on analysis of the mitigation mechanism of instabi...
Open-loop control is known to be an effective strategy for controlling self-excited thermoacoustic o...
The dynamic transition from combustion noise to combustion instability was investigated experimental...
Thermoacoustic systems with a turbulent reactive flow, prevalent in the fields of power and propulsi...
In the context of this work we attempt to examine the intermittency characteristics of thermoacousti...
We investigate the onset of thermoacoustic instabilities in a turbulent combustor terminated with an...
An experimental study on a turbulent, swirl-stabilized backward facing step combustor is conducted t...
A detailed study concerning a novel, dynamic control strategy for mitigating thermoacoustic instabil...
A joint experimental and computational study of thermoacoustic instabilities in a model swirl-stabil...
The thermoacoustic coupling caused by dynamic flow/flame interactions was investigated in a gas-turb...
Turbulent premixed flames often experience thermoacoustic instabilities when the combustion heat rel...
This experimental study focuses on characterizing the nonlinear combustion dynamics prior to blowout...
Self-exited thermoacoustic instability is undesirable in gas turbines and other propulsion systems ...
This thesis was awarded the Leonardo da Vinci prize in 2013 for outstanding doctoral research in flu...
Thermoacoustic instability in a lean premixed combustor is a major impediment towards reliable opera...