Implications of unsteady analytical flowfields on rocket combustion stability

34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 1998, Pages 1-6

  Majdalani, J ^a   Flandro, G A ^b  

^a Marquette University   (United States)

^b UNIVERSITY OF TENNESSEE SPACE INSTITUTE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION; FLOW FIELDS; PROPELLANTS; PROPULSION; ROCKET ENGINES; ROCKETS; SYSTEM STABILITY; VELOCITY;

ANALYTICAL FORMULATION; COMBUSTION STABILITY; COMPUTATIONAL DATA; MOMENTUM CONSERVATIONS; NUMERICAL COMPARISON; PROPELLANT SURFACES; SOLID ROCKET MOTORS; VELOCITY COMPONENTS;

NAVIER STOKES EQUATIONS;

EID: 84963804651     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. landro, 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. Flandro, G. A., “Effects of Vorticity on Rocket Combustion Stability,” Journal of Propulsion and Power, Vol. 11, No. 4, 1995, pp. 607-625.
5. 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.
6. 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.
7. 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.
8. Bosley, D. L., “A Technique for the Numerical Verification of Asymptotic Expansions,” SIAM Review, Vol. 38, No. 1,1996, pp. 128-135.