A numerical method is developed for transient linear analysis of quasi-one-dimensional thermoacoustic systems, with emphasis on stability properties. This approach incorporates the effects of mean flow variation as well as self-excited sources such as the unsteady heat release across a flame. Working in the frequency domain, the perturbation field is represented as a superposition of local wave modes, which enables the linearized equations to be integrated in space. The problem formulation is completed by specifying appropriate boundary conditions. Here, we consider impedance boundary conditions as well as those relevant to choked and shocked flows. For choked flows, the boundary condition follows from the requirement that perturbations remain regular at the sonic point, while the boundary conditions applicable at a normal shock are obtained from the shock jump conditions. The numerical implementation of the proposed formulation is described for the system eigenvalue problem, where the natural modes are sought. The scheme is validated by comparison with analytical and numerical solutions.

1.
Culick
,
F. E. C.
,
1994
, “
Some Recent Results for Nonlinear Acoustics in Combustion Chambers
,”
AIAA J.
,
32
, pp.
146
269
.
2.
Pankiewitz, C., and Sattelmayer, T., 2002, “Time Domain Simulation of Combustion Instabilities in Annular Combustors,” ASME Paper GT-2002-30064.
3.
Cohen
,
J. M.
,
Wake
,
B. E.
, and
Choi
,
D.
,
2003
, “
Investigation of Instabilities in a Lean Premixed Step Combustor
,”
J. Propul. Power
,
19
, pp.
81
88
.
4.
Bloxsidge
,
G. J.
,
Dowling
,
A. P.
, and
Langhorne
,
P. J.
,
1988
, “
Reheat buzz: An Acoustically Coupled Combustion Instability. Part 2. Theory
,”
J. Fluid Mech.
,
193
, pp.
445
473
.
5.
Dowling
,
A. P.
,
1995
, “
The Calculation of Thermoacoustic Oscillations
,”
J. Sound Vib.
,
180
, pp.
557
581
.
6.
Keller
,
J. J.
,
1995
, “
Thermoacoustic Oscillations in Combustion Chambers of Gas Turbines
,”
AIAA J.
,
33
, pp.
2280
2287
.
7.
Stow, S. R., and Dowling, A. P., 2001, “Thermoacoustic Oscillations in an Annular Combustor,” ASME Paper 2001-GT-0037.
8.
Evesque, S., and Polifke, W., 2002, “Low-order Acoustic Modelling for Annular Combustors: Validation and Inclusion of Modal Coupling,” ASME Paper GT-2002-30064.
9.
Marble
,
F. E.
, and
Candel
,
S. M.
,
1977
, “
Acoustic Disturbance from Gas Non-uniformities Convected Through a Nozzle
,”
J. Sound Vib.
,
55
, pp.
225
243
.
10.
Culick
,
F. E. C.
, and
Rogers
,
T.
,
1983
, “
The Response of Normal Shocks in Diffusers
,”
AIAA J.
,
21
, pp.
1382
2390
.
11.
Whitham, G. B., 1974, Linear and Nonlinear Waves (Wiley, New York).
12.
Tam
,
C. K. W.
, and
Hu
,
F. Q.
,
1989
, “
On the Three Families of Instability Waves of High-Speed Jets
,”
J. Fluid Mech.
,
201
, pp.
447
483
.
13.
Kuo
,
C.-Y.
, and
Dowling
,
A. P.
,
1996
, “
Oscillations of a Moderately Underexpanded Choked Jet Impinging Upon a Flat Plate
,”
J. Fluid Mech.
,
315
, pp.
267
291
.
14.
Munjal, M. L., 1987, Acoustics of Ducts and Mufflers with Application to Exhaust and Ventilation System Design (Wiley, New York).
15.
Prasad
,
D.
, and
Feng
,
J.
,
2004
, “
Thermoacoustic Stability of Quasi-One-Dimensional Flows. Part II Application to Basic Flows
,”
J. Turbomach
,
126
, pp.
644
652
.
16.
Lin, R.-S., “Entropy Driven Thermoacoustic Instability,” (unpublished).
You do not currently have access to this content.