Yang, Vigor and Culick, Fred E. C. (1987) Third-order nonlinear acoustic waves and triggering of pressure oscillations in combustion chambers. Part I: Longitudinal modes. AIAA Papers, AIAA-87-1873 . American Institute of Aeronautics and Astronautics . http://resolver.caltech.edu/CaltechAUTHORS:20101203-142326424
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An analytical analysis has been developed to investigate the behavior of unsteady motions in combustion chambers. The model accommodates the third-order nonlinear acoustics and a second-order combustion response. Ths influences of various linear and nonlinear parameters on the limit cycles and triggering of pressure osoillations are disoussed in detail. Results indicate that the third-order acoustics has little influence on the triggering of instability. It only affects the limiting amplitudes and the stability domains of limit cycles. The nonlinear combustion response plays an essential role in determining the characteristics of triggering.
|Item Type:||Report or Paper (Report)|
|Additional Information:||© 1987, American Institute of Aeronautics and Astronautics. This work was supported partly by the Office of Naval Research, Grant No. 00014-84-K-0434, and partly by The Pennsylvania State University. The authors are greatly indebted to Dr. H. S. Sun for his assistance in formulating the model of the third-order nonlinear acoustic model.|
|Group:||Guggenheim Jet Propulsion Center, GALCIT|
|Other Numbering System:|
|Official Citation:||Third-order nonlinear acoustic waves and triggering of pressure oscillations in combustion chambers. Part I: Longitudinal modes YANG, VIGOR, Pennsylvania State University, University Park; CULICK,FRED E. C., California Institute of Technology, Pasadena AIAA-1987-1873 SAE, ASME, and ASEE, Joint Propulsion Conference, 23rd, San Diego, CA, June 29-July 2, 1987|
|Usage Policy:||No commercial reproduction, distribution, display or performance rights in this work are provided.|
|Deposited By:||Ruth Sustaita|
|Deposited On:||04 Dec 2010 00:14|
|Last Modified:||22 Sep 2016 21:52|
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