TY - GEN
T1 - Uncertainty quantification of flame transfer function under a bayesian framework
AU - Li, Yixing
AU - Wang, Xingjian
AU - Mak, Simon
AU - Sung, Chih Li
AU - Jeff Wu, C. F.
AU - Yang, Vigor
N1 - Funding Information:
This work was sponsored partly by the Air Force Office of Scientific Research under Grant No. FA 9550-10-1-0179, and partly by the William R. T. Oakes Endowment of the Georgia Institute of Technology. The authors gratefully acknowledge support and advice given by Dr. Mitat A. Birkan.
PY - 2018
Y1 - 2018
N2 - Combustion instability identification techniques have received increasing attentions in the design and development of modern propulsion systems, and one of the most popular approaches is the flame transfer function (FTF). This work proposes a novel method to identify the uncertainty quantification (UQ) of FTF. The method is composed of two steps. First, Bayesian approach is applied to model the UQ of impulse function. After the application of prior distributions to impulse function and its variance, the distributions are gradually updated to posterior distributions through incorporation of observed data. Sampling is then drawn from the posterior distributions. For the second step, the uncertainty of impulse function propagates forward to determine the UQ of FTF, through propagation in each sample. This Bayesian approach is then applied to study the combustion dynamics of four liquid-oxygen/kerosene bi-swirl injectors at supercritical conditions. This novel approach is able to capture dominant responses of four injectors, which is characterized by vortex shedding. Not limited to good estimations of impulse functions and FTFs, this method also describes how certain we are of such an estimate. The ranges of uncertainty are small at dominant frequencies and large otherwise, indicating that the dominant responses is unaffected by noise. This method is able to capture dominant responses of four injectors, which is characterized by vortex shedding. This study provides novel perspectives on both transfer function identification and UQ estimation, and will serve as a benchmark for the future analyses of FTF and combustion instability.
AB - Combustion instability identification techniques have received increasing attentions in the design and development of modern propulsion systems, and one of the most popular approaches is the flame transfer function (FTF). This work proposes a novel method to identify the uncertainty quantification (UQ) of FTF. The method is composed of two steps. First, Bayesian approach is applied to model the UQ of impulse function. After the application of prior distributions to impulse function and its variance, the distributions are gradually updated to posterior distributions through incorporation of observed data. Sampling is then drawn from the posterior distributions. For the second step, the uncertainty of impulse function propagates forward to determine the UQ of FTF, through propagation in each sample. This Bayesian approach is then applied to study the combustion dynamics of four liquid-oxygen/kerosene bi-swirl injectors at supercritical conditions. This novel approach is able to capture dominant responses of four injectors, which is characterized by vortex shedding. Not limited to good estimations of impulse functions and FTFs, this method also describes how certain we are of such an estimate. The ranges of uncertainty are small at dominant frequencies and large otherwise, indicating that the dominant responses is unaffected by noise. This method is able to capture dominant responses of four injectors, which is characterized by vortex shedding. This study provides novel perspectives on both transfer function identification and UQ estimation, and will serve as a benchmark for the future analyses of FTF and combustion instability.
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U2 - 10.2514/6.2018-1187
DO - 10.2514/6.2018-1187
M3 - Conference contribution
AN - SCOPUS:85044480738
SN - 9781624105241
T3 - AIAA Aerospace Sciences Meeting, 2018
BT - AIAA Aerospace Sciences Meeting
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Aerospace Sciences Meeting, 2018
Y2 - 8 January 2018 through 12 January 2018
ER -