Published January 1987 | Version Published
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Longitudinal Mode Combustion Instabilities in a Dump Combustor

Abstract

The mechanism by which longitudinal modes of a dump combustor are excited has been investigated. The unsteady combustion is a result of the shedding of large scale vortical structures from the flameholder. Driving and damping as determined by Rayleigh's criterion were investigated by using the cross-spectrum and phase of the fluctuating pressure and radiation intensity signals at various locations in the combustor. Thus, the excitation of a particular mode was found to depend on the pressure mode shape and the magnitude and phase of the velocity fluctuation at the flameholder. Fluid mechanical mixing and the chemical reaction rate of the fuel also effect the distribution of heat release and hence the locations of driving and damping. Finally, a mechanism for existence of the limit cycle is discussed.

Additional Information

© American Institute of Aeronautics and Astronautics, Inc., 1987. Financial support for this work was provided under AFOSR Grant No. 84-0286.

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Identifiers

Eprint ID
21106
Resolver ID
CaltechAUTHORS:20101202-073712764

Funding

Air Force Office of Scientific Research (AFOSR)
84-0286

Dates

Created
2010-12-04
Created from EPrint's datestamp field
Updated
2019-10-03
Created from EPrint's last_modified field

Caltech Custom Metadata

Caltech groups
Guggenheim Jet Propulsion Center
Series Name
AIAA Papers
Series Volume or Issue Number
AIAA-87-0220
Other Numbering System Name
AIAA
Other Numbering System Identifier
87-0220