An investigation of droplet breakup in a high mach, low Weber number regime

41st Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2003, Pages

  Dinh, T N ^a   Li, G J ^a   Theofanous, T G ^a  

^a UNIVERSITY OF CALIFORNIA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; AIRCRAFT ENGINES; COMBUSTION KNOCK; DENSITY OF GASES; DETONATION; FLOW OF GASES; FUEL SYSTEMS; FUELS;

DETONATION ENGINES; DROPLET BREAKUP; EXPERIMENTAL APPROACHES; EXPERIMENTAL FACILITIES; FUEL DROPLETS; RAREFIED GAS; SUPERSONIC GAS FLOWS; WEBER NUMBERS;

DROP BREAKUP;

EID: 85088342265     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-317     Document Type: Conference Paper

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