Acoustic analysis of hybrid rocket combustion chambers

Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference

Volumn 4, Issue , 2007, Pages 3609-3617

  Pastrone, Dario ^a,c,d   Casalino, Lorenzo ^a,c,d   Sentinella, Matteo Rosa ^a,c   Carmicino, Carmine ^b,d,e,f  

^a POLITECNICO DI TORINO   (Italy)

^b UNIVERSITY OF NAPLES FEDERICO II   (Italy)

^c Departimento di Energetica   (Italy)

^d AIAA   (United States)

^e Dipartimento di Ingegneria Aerospaziale   (Italy)

^f ITALIAN AEROSPACE RESEARCH CENTER   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC ANALYSIS; ACOUSTIC MOTIONS; COMBUSTION DYNAMICS;

COMBUSTION CHAMBERS; LINEAR STABILITY ANALYSIS; MEASUREMENT THEORY; MOMENTUM; PRESSURE EFFECTS;

ROCKETS;

EID: 36749069850     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (16)

1. Karabeyouglu, A., De Zilwa, S., Cantwell, B., and Zilliac, G., "Modeling of Hybrid Rocket Low Frequency Instabilities," Journal of Propulsion and Power, Vol. 21, No. 6, 2005, pp. 1107-1116.
2. De Zilwa, S., Zilliac, G., Reinath, M., and Karabeyoglu, A., "Time-Resolved Fuel-Grain Port Diameter Measurement in Hybrid Rocket," Journal of Propulsion and Power, Vol. 20, No. 4, 2004, pp. 684-689.
3. Hessler, R. O., "Passive Linear Stability Measurements," JANNAF Combustion Meeting, West Palm Beach, FL, October 1997.
4. Culick, F. E. C., "Combustion Instabilities: Mating Dance of Chemical, Combustion, and Combustor Dynamics," Paper AIAA 2000-3178, July 2000.
5. Hessler R. O. et alii, "Acoustic Response of a Model Rocket Chamber," Second European Conference on Launcher Technology: Space Solid Propulsion, Rome, Italy, November 2000.
6. Pastrone, D., Saretto, S.R., and Vassallo, E., "Acoustic Analysis of a Subscale Rocket Motor," Paper AIAA 2001-3867, July 2001.
7. Pastrone, D., and Saretto, S.R., "An Improved Acoustic Analysis of a Subscale Rocket Motor", Paper AIAA-2003-4627, July 2003.
8. Carmicino, C., and Russo Sorge, A., "The Effects of Oxidizer Injector Design on Hybrid Rockets Combustion Stability", Paper AIAA 2006-4677, July 2006.
9. Carmicino, C., and Russo Sorge, A., "Influence of a Conical Axial Injector on Hybrid Rocket Performance," Journal of Propulsion and Power, Vol. 22, No. 5, 2006, pp. 984-995
10. Carmicino, C., and Russo Sorge, A., "Performance Comparison Between Two Different Injector Configurations in a Hybrid Rocket", Aerospace Science and Technology, Vol. 11, No. 1, 2007, pp. 61-67.
11. Dènos, R., and Olivari, D., "Digital Data Acquisition and Processing," Measurement Techniques in Fluid Dynamics. An Introduction, von Karman Institute for Fluid Dynamics, 2nd ed. Revised, 2001.
12. Qian, S., and Chen, D., Joint Time-Frequency Analysis - Methods and Applications, Prentice Hall PTR, 1996
13. Bussi, G., Colasurdo, G. and Pastrone, D., "Nozzle Effects on Linear Stability Behaviour of Combustors," Paper ISABE 93-7044, September 1993.
14. Carmicino, C., and Russo Sorge, A., "Role of Injection in Hybrid Rockets Regression Rate Behavior," Journal of Propulsion and Power, Vol. 21, No. 4, 2005, pp. 606-612
15. Micci, M. M., Caveny, L. H., and Sirignano, W. A., "Linear Analysis of Forced Longitudinal Waves in Rocket Motor Chambers," AIAA Journal, Vol. 19, No. 2, 1981, pp. 198-204.
16. Colasurdo, G., and Pastrone, D., "Indirect Oprimization Method for Impulsive Transfer," AIAA Paper 94-3762, Aug. 1994.