Yang, V. and Kim, S. I. and Culick, F. E. C. (1988) Third-Order Nonlinear Acoustic Instabilities in Combustion Chambers, Part II: Transverse Modes. AIAA Papers, AIAA-88-0152 . American Institute of Aeronautics and Astronautics . http://resolver.caltech.edu/CaltechAUTHORS:20101203-144226944
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An analytical analysis has been developed to investigate the behavior of unsteady transverse pressure oscillations in combustion chambers. The model extends the previous analysis for the second-order standing wave motions and accommodates spinning oscillations and third-order nonlinearities. The influences of various parameters and initial conditions on the limit cycles and triggering of pressure oscillations are discussed. Results indicate that the existence of spinning oscillations depends strongly on the number of modes included in the analysis and on the initial conditions. The third-order acoustics has little influence on the triggering of instability. It only modifies the characteristics of limiting amplitudes.
|Item Type:||Report or Paper (Report)|
|Additional Information:||© 1988, American Institute of Aeronautics and Astronautics. This work was supported partly by the ONR 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|
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|Official Citation:||Third-order nonlinear acoustic instabilities in combustion chambers.II - Transverse modes YANG, VIGOR, Pennsylvania State University, University Park; CULICK,FRED E. C., California Institute of Technology, Pasadena AIAA-1988-152 Aerospace Sciences Meeting, 26th, Reno, NV, Jan 11-14, 1988.|
|Usage Policy:||No commercial reproduction, distribution, display or performance rights in this work are provided.|
|Deposited By:||Ruth Sustaita|
|Deposited On:||04 Dec 2010 00:12|
|Last Modified:||25 Mar 2014 04:31|
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