TY - GEN
T1 - Bifurcation measurement and analysis of a nonlinear Rijke-type thermoacoustic system
AU - Zhao, Dan
AU - Li, Xinyan
N1 - Publisher Copyright:
© 2018 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
PY - 2018
Y1 - 2018
N2 - Thermoacoustic systems are typically nonlinear, which are characterized by limit cycle pressure oscillations. In present work, we conduct bifurcation analysis to a nonlinear thermoacoustic system by using the method of multiple scales to gain insight on the system's asymptotic behaviors. Both theoretical and experimental studies are performed. To de- scribe/characterize the unsteady heat release from an acoustically compact heat source in the system, two different models are proposed to approximate experimental measurements. Model A is formulated with 3rd order polynomial equation, while model B is 5th order one. Comparison is made between the results obtained from these two models. Model A is shown to be associated with supercritical Hopf bifurcation. However, subcritical Hopf bifurcation occurs in the higher-order nonlinear thermoacoustic system, i.e. model B. Furthermore, hysteresis and bistable zones are observed. In addition, the effects of 1) the heating power K, 2) the axial location of the heat source xf/L and 3) the overall acoustic damping/loss ξ on supercritical and subcritical bifurcation are studied one at a time. To validate our theoretical findings on supercritical and subcritical bifurcation, experimental investigation on a Rijke tube is conducted. Both super- and subcritical bifurcation are experimentally observed, as the fuel flow rate mf or the flame axial location xf/L is varied. The experimental measurements are more consistent with the prediction from Model B. This confirms that it is more accurate to predict subcritical bifurcation behaviors by modelling the thermoacoustic system with a higher order nonlinear model.
AB - Thermoacoustic systems are typically nonlinear, which are characterized by limit cycle pressure oscillations. In present work, we conduct bifurcation analysis to a nonlinear thermoacoustic system by using the method of multiple scales to gain insight on the system's asymptotic behaviors. Both theoretical and experimental studies are performed. To de- scribe/characterize the unsteady heat release from an acoustically compact heat source in the system, two different models are proposed to approximate experimental measurements. Model A is formulated with 3rd order polynomial equation, while model B is 5th order one. Comparison is made between the results obtained from these two models. Model A is shown to be associated with supercritical Hopf bifurcation. However, subcritical Hopf bifurcation occurs in the higher-order nonlinear thermoacoustic system, i.e. model B. Furthermore, hysteresis and bistable zones are observed. In addition, the effects of 1) the heating power K, 2) the axial location of the heat source xf/L and 3) the overall acoustic damping/loss ξ on supercritical and subcritical bifurcation are studied one at a time. To validate our theoretical findings on supercritical and subcritical bifurcation, experimental investigation on a Rijke tube is conducted. Both super- and subcritical bifurcation are experimentally observed, as the fuel flow rate mf or the flame axial location xf/L is varied. The experimental measurements are more consistent with the prediction from Model B. This confirms that it is more accurate to predict subcritical bifurcation behaviors by modelling the thermoacoustic system with a higher order nonlinear model.
UR - http://www.scopus.com/inward/record.url?scp=85051295903&partnerID=8YFLogxK
U2 - 10.2514/6.2017-3214
DO - 10.2514/6.2017-3214
M3 - Conference contribution
AN - SCOPUS:85051295903
SN - 9781624105609
T3 - 2018 AIAA/CEAS Aeroacoustics Conference
BT - 2018 AIAA/CEAS Aeroacoustics Conference
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA/CEAS Aeroacoustics Conference, 2018
Y2 - 25 June 2018 through 29 June 2018
ER -