Leading-edge flame detachment: Effect on pressure-coupled combustion response

Journal of Propulsion and Power

Volumn 14, Issue 2, 1998, Pages 160-165

  Beiter, C A ^a,b,c   Price, E W ^a,c  

^a Georgia Institute of Technology   (United States)

^b US Army For Sci Technol Ctr   (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION; FLAME RESEARCH; PRESSURE EFFECTS;

COMPOSITE PROPELLANTS; LEADING EDGE FLAME DETACHMENT; PRESSURE COUPLED COMBUSTION RESPONSE;

SOLID PROPELLANTS;

EID: 0032026211     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.5281     Document Type: Article

References (10)

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3. Beiter, C. A., "The Role of Combustion Zone Microstructure on the Pressure-Coupled Response of Composite Propellants," Ph.D. Dissertation, Georgia Inst. of Technology, Atlanta, GA, May 1991.
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9. Mathes, H. B., "A Facility for Testing the Acoustic Combustion Instability," Proceedings of the 26th International Symposium, Instrumentation in the Aerospace Industry, Vol. 26, Instrument Society of America, Research Triangle Park, NC, 1980, pp. 376-378; also Advances in Test Measurement, Vol. 17, 1980, pp. 367-378.
10. Culick, F. E. C., "Report of the Committee on Standardization of Combustion Instability Measurements in the T-Burner," Chemical Propulsion Information Agency, Publication 191, Columbia, MD, Nov. 1969.