Ignition of cryogenic H2/LOX sprays

Aerospace Science and Technology

Volumn 7, Issue 7, 2003, Pages 517-531

  Gurliat, O ^b   Schmidt, V ^a   Haidn, O J ^a   Oschwald, M ^a  

^a SNECMA   (France)

^b GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

Cryogenic spray; Flame propagation; Hydrogen; Ignition; Liquid rocket engine; LOX; Shear coaxial injector

Indexed keywords

ATOMIZATION; CRYOGENIC LIQUIDS; FLAME RESEARCH; FLOW VISUALIZATION; LASER APPLICATIONS; LIQUID PROPELLANTS; PRESSURE EFFECTS; PULSED LASER APPLICATIONS; REYNOLDS NUMBER; ROCKET ENGINES; VELOCITY MEASUREMENT;

CRYOGENIC SPRAYS; FLAME PROPAGATION; SHEAR COAXIAL INJECTORS;

IGNITION;

EID: 0346724376     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1270-9638(03)00059-2     Document Type: Article

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