Published June 1991 | Version Published
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Characterization and modeling of aperiodic pressure oscillations in combustion chambers

Abstract

Classification of the long-term dynamical behavior of pressure oscillations in a laboratory combustion chamber has been performed using methods of modern dynamical systems theory. The method involves the construction of a phase-space representation from a single pressure record or time series using the time-delay embedding method. The pointwise correlation dimension of the resulting attractor in phase-space provides a lower bound on the number of modes that participate in the oscillations. The results show that the oscillations are quasiperiodic with a dimension near two over an order of magnitude of amplitudes. Quasiperiodicity is a result of the incommensurate frequencies of the system acoustic modes. A model for the dynamics is constructed by converting the governing equations to a kicked-oscillator model. When compared with the experimental data, the model results have similar pressure and velocity spectra and the attractor dimension verifies that quasiperiodic oscillations are present.

Additional Information

© 1991, AIAA. For permission to copy or republish, contact American Institute of Aeronautics and Astronautics. Lecturer in Jet Propulsion, Member AIAA

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Identifiers

Eprint ID
21057
Resolver ID
CaltechAUTHORS:20101130-100452033

Dates

Created
2010-12-10
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Updated
2019-10-03
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Caltech Custom Metadata

Caltech groups
Guggenheim Jet Propulsion Center
Series Name
AIAA Papers
Series Volume or Issue Number
AIAA 91-2082
Other Numbering System Name
AIAA
Other Numbering System Identifier
91-2082