TY - GEN
T1 - Bifurcation measurement and analysis of a nonlinear rijke-type thermoacoustic system
AU - Li, Xinyan
AU - Zhao, Dan
AU - Li, Shen
N1 - Publisher Copyright:
© 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2017
Y1 - 2017
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 describe/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 m˙ f 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 describe/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 m˙ f 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=85023639388&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:85023639388
SN - 9781624105043
T3 - 23rd AIAA/CEAS Aeroacoustics Conference, 2017
BT - 23rd AIAA/CEAS Aeroacoustics Conference, 2017
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 23rd AIAA/CEAS Aeroacoustics Conference, 2017
Y2 - 5 June 2017 through 9 June 2017
ER -