Convergence of Two Analytical Flowfield Models Predicting a Destabilizing Agent in Rocket Combustion

Journal of Propulsion and Power

Volumn 16, Issue 3, 2000, Pages 492-497

  Majdalani, J ^a   Flandro, G A ^b   Roh, T S ^c  

^a MARQUETTE UNIVERSITY   (United States)

^b UNIVERSITY OF TENNESSEE SPACE INSTITUTE   (United States)

^c CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0000595536     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.5595     Document Type: Article

References (12)

1. Flandro, G. A., "On Flow Turning," AIAA Paper 95-2530, July 1995.
2. Majdalani, J., and Van Moorhem, W. K., "Improved Time-Dependent Flowfield Solution for Solid Rocket Motors," AIAA Journal, Vol. 36, No. 2, 1998, pp. 241-248.
3. Majdalani, J., "Characterization of the Laminar Boundary Layer in Solid Rocket Motors," AIAA Paper 98-3699, July 1998.
4. Majdalani, J., "The Boundary Layer Structure in Cylindrical Rocket Motors," AIAA Journal, Vol. 37, No. 4, 1999, pp. 505-508.
5. Flandro, G. A., "Effects of Vorticity on Rocket Combustion Stability," Journal of Propulsion and Power, Vol. 11, No. 4, 1995, pp. 607-625.
6. Culick, F. E. C., "Rotational Axisymmetric Mean Flow and Damping of Acoustic Waves in a Solid Propellant Rocket," AIAA Journal, Vol. 4, No. 8, 1966, pp. 1462-1464.
7. Chu, B. T., and Kovásznay, L. S. G., "Nonlinear Interactions in a Viscous Heat-Conducting Compressible Gas," Journal of Fluid Mechanics, Vol. 3, 1957, pp. 494-514.
8. Carrier, B. T., and Carlson, F. D., "On the Propagation of Small Disturbances in a Moving Compressible Fluid," Quarterly of Applied Mathematics, Vol. 4, No. 1, 1946, pp. 1-12.
9. Flandro, G. A., "Effects of Vorticity Transport on Axial Acoustic Waves in a Solid Propellant Rocket Chamber," Combustion Instabilities Driven by Thermo-Chemical Acoustic Sources, edited by A. S. Hersh, I. Catton, and R. F. Keltie, Noise Control and Acoustics, Vol. 4, American Society of Mechanical Engineers, New York, 1989, pp. 53-61.
10. Roh, T. S., Tseng, I. S., and Yang, V., "Effects of Acoustic Oscillations on Flame Dynamics of Homogeneous Propellants in Rocket Motors," Journal of Propulsion and Power, Vol. 11, No. 4, 1995, pp. 640-650.
11. Roh, T. S., and Culick, F. E. C., "Transient Combustion Response of Homogeneous Propellants to Acoustic Oscillations in Axisymmetric Rocket Motors," AIAA Paper 97-3325, July 1995.
12. Bosley, D. L., "A Technique for the Numerical Verification of Asymptotic Expansions," SIAM Review, Vol. 38, No. 1, 1996, pp. 128-135.