Effects of boundary layers and wakes on shock-flame interactions and DDT

40th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2002, Pages

  Oran, E S ^a   Gamezo, V N ^a   Khokhlov, A M ^a  

^a NAVAL RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; BIFURCATION (MATHEMATICS); BOUNDARY LAYERS; COMBUSTION; DETONATION; ETHYLENE; NAVIER STOKES EQUATIONS; SHOCK TUBES; WAKES;

CELLULAR DETONATION; COMPLEX SEQUENCES; COMPUTATIONAL MESH; DEFLAGRATION TO DETONATION TRANSITION; FLAME ACCELERATIONS; RE-CIRCULATION FLOW; SHOCK TUBE EXPERIMENT; VELOCITY GRADIENTS;

FLAME RESEARCH;

EID: 85086612261     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-776     Document Type: Conference Paper

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