Effects of NOx and HO2 on plasma ignition in a supersonic flow

A Collection of Technical Papers - 14th AIAA/AHI International Space Planes and Hypersonic Systems and Technologies Conference

Volumn 1, Issue , 2006, Pages 631-638

  Abe, Naoyuki ^a,c   Ohashi, Ryuta ^a,c   Takita, Kenichi ^a,c,d   Masuya, Goro ^a,c,d   Ju, Yiguang ^b,c,d  

^a TOHOKU UNIVERSITY   (Japan)

^b Princeton University   (United States)

^c Department of Aeronautics and Space Engineering ^*

^d AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CATALYTIC REACTIONS; IGNITION TESTS; STATIC PRESSURE; THRESHOLD PRESSURE;

COMPUTER SIMULATION; CONCENTRATION (PROCESS); HYDROCARBONS; IGNITION; PLASMAS; SUPERSONIC FLOW;

HYDROGEN;

EID: 33947269229     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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