Utility of computational modeling for the study of combustion instability in small MMH-NTO liquid rocket engines

Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference

Volumn 5, Issue , 2007, Pages 5370-5380

  Nusca, Michael J ^a,b  

^a U S ARMY RESEARCH LABORATORY   (United States)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION INSTABILITY; FLIGHT TESTING; FLOW PHYSICS; THRUST LEVELS;

COMBUSTION EQUIPMENT; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; DROP FORMATION; MISSILES;

ROCKET ENGINES;

EID: 36749082935     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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