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.
Skip Nav Destination
Article navigation
October 2004
Technical Papers
Thermoacoustic Stability of Quasi-One-Dimensional Flows–Part I: Analytical and Numerical Formulation
Dilip Prasad,
Dilip Prasad
Aerodynamics Division, Pratt & Whitney Aircraft Engines, East Hartford, CT 06108
Search for other works by this author on:
Jinzhang Feng
Jinzhang Feng
Aerodynamics Division, Pratt & Whitney Aircraft Engines, East Hartford, CT 06108
Search for other works by this author on:
Dilip Prasad
Aerodynamics Division, Pratt & Whitney Aircraft Engines, East Hartford, CT 06108
Jinzhang Feng
Aerodynamics Division, Pratt & Whitney Aircraft Engines, East Hartford, CT 06108
Contributed by the International Gas Turbine Institute (IGTI) of THE AMERICAN SOCIETY OF MECHANICAL ENGINEERS for publication in the ASME JOURNAL OF TURBOMACHINERY. Paper presented at the International Gas Turbine and Aeroengine Congress and Exhibition, Vienna, Austria, June 13–17, 2004, Paper No. 2004-GT-53943. Manuscript received by IGTI, October 1, 2003; final revision March 1, 2004. IGTI Review Chair: A. J. Strazisar.
J. Turbomach. Oct 2004, 126(4): 637-644 (8 pages)
Published Online: December 29, 2004
Article history
Received:
October 1, 2003
Revised:
March 1, 2004
Online:
December 29, 2004
Citation
Prasad , D., and Feng, J. (December 29, 2004). "Thermoacoustic Stability of Quasi-One-Dimensional Flows–Part I: Analytical and Numerical Formulation ." ASME. J. Turbomach. October 2004; 126(4): 637–644. https://doi.org/10.1115/1.1791288
Download citation file:
Get Email Alerts
Cited By
Related Articles
Analysis of Thin Film Flows Using a Flux Vector Splitting
J. Fluids Eng (March,2003)
Assessment of Very High Order of Accuracy in Implicit LES models
J. Fluids Eng (December,2007)
Online Monitoring of Thermoacoustic Eigenmodes in Annular Combustion Systems Based on a State-Space Model
J. Eng. Gas Turbines Power (February,2017)
Optimal Shape of a Rotating Rod With Unsymmetrical Boundary Conditions
J. Appl. Mech (November,2007)
Related Proceedings Papers
Related Chapters
Stable Analysis on Speed Adaptive Observer in Low Speed Operation
International Conference on Instrumentation, Measurement, Circuits and Systems (ICIMCS 2011)
Multiple Positive Solutions for General Sturm-Liouville Boundary Value Problems on the Half-Line
International Conference on Information Technology and Computer Science, 3rd (ITCS 2011)
The Solutions for Semi-Positone Boundary Value Problems with Linear Functional Boundary Conditions on the Half-Line
International Conference on Information Technology and Computer Science, 3rd (ITCS 2011)