NASA NTRS · 20050182054
Control of Combustion-Instabilities Through Various Passive Devices
Abstract
Results of a computational study on the effectiveness of various passive devices for the control of combustion instabilities are presented. An axi-symmetric combustion chamber is considered. The passive control devices investigated are, baffles, Helmholtz resonators and quarter-waves. The results show that a Helmholtz resonator with a smooth orifice achieves the best control results, while a baffle is the least effective for the frequency tested. At high sound pressure levels, the Helmholtz resonator is less effective. It is also found that for a quarter wave, the smoothness of the orifice has the opposite effect than the Helmholtz resonator, i.e. results in less control.
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Frendi, Abdelkader, Nesman, Tom, Canabal, Francisco. 2005-01-01. Control of Combustion-Instabilities Through Various Passive Devices. https://ntrs.nasa.gov/citations/20050182054
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