Modeling the effect of unsteady chamber conditions on atomization processes

Journal of Propulsion and Power

Volumn 14, Issue 4, 1998, Pages 576-579

  Rump, K M ^a,b,c   Heister, S D ^a,c  

^a PURDUE UNIVERSITY   (United States)

^b BOEING COMPANY   (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ATOMIZATION; BOUNDARY ELEMENT METHOD; COMBUSTION; COMBUSTION CHAMBERS; COMPUTER SIMULATION; LIQUID PROPELLANTS; NOZZLES; ORIFICES; PRESSURE EFFECTS; UNSTEADY FLOW;

WEBER NUMBER;

ROCKET ENGINES;

EID: 0032116196     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.7645     Document Type: Article

References (5)

1. Bazarov, V. G., "Influence of Propellant Injector Stationary and Dynamic Parameters on High Frequency Combustion Stability," AIAA Paper 96-3119, July 1996.
2. Jensen, R. (ed.), "JANNAF Subcommittee on Combustion Stability - Annual Report," 27th JANNAF Combustion Meeting, Cheyenne, Wyoming, 1990.
3. Reba, I., and Brosilow, C., "Combustion Instability: Liquid Stream and Droplet Behavior," Wright Air Development Center, TR 59-720, May 1960.
4. Hilbing, J. H., Heister, S. D., and Spangler, C. A., "A Boundary Element Method for Atomization of a Finite Liquid Jet," Atomization and Sprays, Vol. 5, No. 6, 1995, pp. 621-638.
5. Rump, K., "Modeling the Effect of Unsteady Chamber Conditions on Atomization Processes," M.S. Thesis, Purdue Univ., West Lafayette, IN, 1996.