Effects of GH2/LOX velocity and momentum ratios on shear coaxial injector atomization

Journal of Propulsion and Power

Volumn 18, Issue 1, 2002, Pages 209-211

  Ferraro, M ^a   Kujala, R J ^a   Thomas, J L ^a   Glogowski, M J ^a   Micci, M M ^a  

^a PENNSYLVANIA STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ATOMIZATION; COMBUSTION; FUEL INJECTION; LIQUID PROPELLANTS; SPACE SHUTTLES;

SHEAR COAXIAL INJECTORS;

COMBUSTION CHAMBERS;

EID: 0036158379     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.5920     Document Type: Article

References (5)

1. Experimental investigation of rocket injector atomization
2. Shear coaxial injector instability mechanisms
3. Shear coaxial injector atomization phenomena for combusting and non-combusting conditions
4. CET93 and CETPC. An interim updated version of the nasa lewis computer program for calculating complex chemical equilibria with applications
5. Supercritical vaporization of liquid oxygen droplets in hydrogen and water environments