Effects of fuel preinjection on mixing in Mach 1.6 airflow

Journal of Propulsion and Power

Volumn 17, Issue 3, 2001, Pages 605-610

  Owens, M ^a   Mullagiri, S ^a   Segal, C ^a   Vinogradov, V A ^b  

^a University of Florida   (United States)

^b CENTRAL INSTITUTE OF AVIATION MOTORS   (Russian Federation)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION; ETHYLENE; HYPERSONIC FLOW; JETS;

COMBUSTION CHAMBER MIXING; GASEOUS ETHYLENE;

SUPERSONIC FLOW;

EID: 0035331614     PISSN: 07484658     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.5784     Document Type: Article

References (12)

1. Supersonic combustion ramjet research at Langley
2. Effect of injection angle on liquid injection into supersonic flow
3. Evaluation of parallel injector configurations for Mach 2 combustion
4. Shock enhancement and control of hypersonic mixing and combustion
5. Injection of liquid into the strut shadow at supersonic velocities
6. Penetration and spreading of liquid jets in an external-internal compression inlet
7. Flameholding configurations for kerosene combustion in a Mach 1.8 airflow
8. Development of an experimentally-flexible facility for mixing-combustion interactions in supersonic flow
9. Injection of bubbling liquid jets from multiple injectors into a supersonic stream
10. Combustion stability limits of hydrogen in a non-premixed supersonic flow