NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Control of Combustion-Instabilities Through Various Passive DevicesResults 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.
Document ID
20050182054
Acquisition Source
Headquarters
Document Type
Preprint (Draft being sent to journal)
Authors
Frendi, Abdelkader
(Alabama Univ. Huntsville, AL, United States)
Nesman, Tom
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Canabal, Francisco
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2005
Subject Category
Acoustics
Meeting Information
Meeting: 11th AIAA/CEAS Aeroacoustic Conference
Location: Monterey, CA
Country: United States
Start Date: May 23, 2005
End Date: May 25, 2005
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available