TY - GEN
T1 - Low-order network model of a duct with non-uniform cross-section and varying mean temperature in the presence of mean flow
AU - Schaefer, F.
AU - Polifke, W.
N1 - Publisher Copyright:
© 2019 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
PY - 2019
Y1 - 2019
N2 - Stability analysis of thermoacoustic systems is often carried out with low-order network models. This paper introduces a method to include a duct element with varying cross-sectional area and an arbitrary mean temperature profile in a thermoacoustic network model. Based on the quasi one-dimensional form of the linearized Euler equations (LEEs) for a perfect, inviscid gas, the system equations are formulated in a state space framework in terms of the Riemann invariants f and g. This approach is predicated on one additional assumption, i.e. that the direct impact of entropy fluctuations on the acoustic waves inside the duct is small. A comparison of model results with analytical analysis shows excellent agreement. Eigenvalues are predicted with good accuracy, even for coarse grids. Furthermore, the mode shapes and frequency responses match those found in the literature, demonstrating the validity of the approach.
AB - Stability analysis of thermoacoustic systems is often carried out with low-order network models. This paper introduces a method to include a duct element with varying cross-sectional area and an arbitrary mean temperature profile in a thermoacoustic network model. Based on the quasi one-dimensional form of the linearized Euler equations (LEEs) for a perfect, inviscid gas, the system equations are formulated in a state space framework in terms of the Riemann invariants f and g. This approach is predicated on one additional assumption, i.e. that the direct impact of entropy fluctuations on the acoustic waves inside the duct is small. A comparison of model results with analytical analysis shows excellent agreement. Eigenvalues are predicted with good accuracy, even for coarse grids. Furthermore, the mode shapes and frequency responses match those found in the literature, demonstrating the validity of the approach.
UR - https://www.scopus.com/pages/publications/85095977779
U2 - 10.2514/6.2019-4376
DO - 10.2514/6.2019-4376
M3 - Conference contribution
AN - SCOPUS:85095977779
SN - 9781624105906
T3 - AIAA Propulsion and Energy Forum and Exposition, 2019
BT - AIAA Propulsion and Energy Forum and Exposition, 2019
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Propulsion and Energy Forum and Exposition, 2019
Y2 - 19 August 2019 through 22 August 2019
ER -