On the Existence and Stability of Limit Cycles for Transverse Acoustic Oscillations in a Cylindrical Combustion Chamber. 1: Standing Modes
- Creators
- Yang, Vigor
- Culick, Fred E. C.
Abstract
Nonlinear pressure oscillations in combustion chambers have been studied using an approximate analysis which treats the unsteady motions as a collection of coupled nonlinear oscillators, each corresponding to an acoustic mode of the chamber. Based on spatial and temporal averaging of the conservation equations, the formulation provides a convenient means for analyzing the nonlinear behavior of acoustic wave motions. The work addresses the linear and nonlinear characteristics of transverse acoustic waves in a cylindrical chamber, with attention focused on the conditions for the existence and stability of limit cycles. As a result of the special structure of the equations, both general and precise conclusions can be reached. Explicit results are given for the special cases of two and three standing modes. Spinning wave motions will be treated in a subsequent paper.
Additional Information
© 1990 Gordon and Breach Science Publishers S.A. Received June 9, 1989; in final form February 5, 1990. This work was supported partly by the Department of the Navy, ONR Contract N0014-84-K-0434, and partly by The Pennsylvania State University. The authors are greatly indebted to Dr. S. I. Kim and Mr. W. T. Lee for carrying out the numerical calculations.Additional details
- Eprint ID
- 21037
- Resolver ID
- CaltechAUTHORS:20101129-110317027
- Department of the Navy
- N0014-84-K-0434
- Pennsylvania State University
- Created
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2010-12-03Created from EPrint's datestamp field
- Updated
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2021-11-09Created from EPrint's last_modified field
- Caltech groups
- Guggenheim Jet Propulsion Center, GALCIT
- Other Numbering System Name
- Guggenheim Jet Propulsion Center