Non-Linear Growth and Limiting Amplitude of Acoustic Oscillations in Combustion Chambers

Combustion Science and Technology

Volumn 3, Issue 1, 1971, Pages 1-16

  Culick, F E C ^a  

^a CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ROCKET ENGINES--COMBUSTION CHAMBERS;

EID: 0015052147     PISSN: 00102202     EISSN: 1563521X     Source Type: Journal    
DOI: 10.1080/00102207108952266     Document Type: Article

References (15)

1. Blackman, A. W., 1960, Effect of Non-Linear Losses on the Design of Absorbers for Combustion Instabilities, ARS Journal 30, 1022–1028.
2. Cantrell, R. H. and Hart, R. W., 1964, Interaction between Sound and Flow in Acoustic Cavities: Mass, Momentum, and Energy Considerations, J. Acoust. Soc. of Amer. 36, 697–706.
3. Crocco, L. and Chang, S.-1., 1956, Theory of Combustion Instability in Liquid-Propellant Rocket Motors, AGARDograph No. 8, Butterworth's Scientific Publications, London (1956).
4. Culick, F. E. C., 1966a, Acoustic Oscillations in Solid Propellant Rocket Motors, Astronautica Acta 12, 112–126.
5. Culick, F. E. C., 1966b, Irrotational Flow and Damping of Acoustic Waves in Solid Propellant Rocket Motors, AIAA Journal 4, 1462–1464.
6. Culick, F. E. C., 1970, Stability of Longitudinal Oscillations with Pressure and Velocity Coupling in a Solid Propellant Rocket Motor, (submitted for publication in Combustion Science and Technology).
7. Ingaard, U. and Ising, H., 1967, Acoustic Non-Linearity of an Orifice, J. Acoust, Soc. of Amer. 42, 6–17.
8. Krylov, N. and Bogoliubov, N., 1947, Introduction to Non-Linear Mechanics, Princeton University Press, Princeton, N.J. (1947), pp. 8–12.
9. Micheli, P. L., 1970, private communication: Measurements of Particle Attenuation in a Pulsed T-burner. Aerojet-General Corp., Sacramento, Calif.
10. Mitchell, C. E., Crocco, L., and Sirignano, W. A., 1969, Nonlinear Longitudinal Instability in Rocket Motors with Concentrated Combustion, Combustion Science and Technology, 1, 35–63.
11. Perry, E. H., 1970, Investigations of the T-burner and Its Role in Combustion Instability Studies, Ph.D. Thesis, California Institute of Technology, Pasadena, Calif. (June 1970).
12. Price, E. W., 1970, private communication: Measurements of Particle Attenuation in a Pulsed T-burner. Naval Weapons Center, China Lake, Calif.
13. T-Burner Manual 1969, prepared by the Committee on Standardization of Combustion Instability Measurements in the T-burner, ICRPG Working Group on Solid Propellant Combustion. Chemical Propulsion Information Agency Publication No. 191 (1969).
14. Tonon, T. S. and Sirignano, W. A. 1970, The Non-Linearity of Acoustic Liners with Flow Effects, AIAA 8th Aerospace Sciences Meeting, New York. New York (1970); AIAA Paper No. 70–128.
15. Zinn, B. T. and Saveli, C. T., 1969, A Theoretical Study of Three-Dimensional Combustion Instability in Liquid-Propellant Rocket Engines, Proceedings of the Twelfth International Symposium on Combustion, Williams and Wilkins Co., Baltimore (1969), pp. 139–147.