Nonlinear Energy Transport Between Longitudinal Acoustic Modes in Cylindrical Combustion Chambers
- Creators
- Jahnke, Craig C.
- Culick, F. E. C.
Abstract
The second order nonlinear longitudinal acoustics in a cylindrical combustion chamber are studied for the case of an unstable second mode. A modal analysis is undertaken and a continuation method is used to determine the limit cycle behavior of the time dependent amplitudes of the acoustic modes as functions of the linear stability of the unstable acoustic mode. It is shown that if an insufficient number of modes are included in the truncated system, bifurcations of the primary limit cycle occur. The energy in the limit cycles is analyzed and the bifurcations are shown to occur as a means of increasing the amount of energy transfer out of the unstable acoustic mode and into the stable acoustic modes through the nonlinear terms.
Additional Information
© 1994 American Institute of Aeronautics and Astronautics, Inc.Attached Files
Published - 363_Jahnke_CC_1994.pdf
Files
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Additional details
- Eprint ID
- 20996
- Resolver ID
- CaltechAUTHORS:20101123-135307146
- Created
-
2010-11-24Created from EPrint's datestamp field
- Updated
-
2019-10-03Created from EPrint's last_modified field
- Caltech groups
- Guggenheim Jet Propulsion Center, GALCIT
- Series Name
- AIAA Papers
- Series Volume or Issue Number
- 94-3190
- Other Numbering System Name
- AIAA
- Other Numbering System Identifier
- 94-3190