110 kW new high enthalpy wind tunnel heated by inductively-coupled-plasma

12th AIAA International Space Planes and Hypersonic Systems and Technologies

Volumn , Issue , 2003, Pages

  Ito, Takeshii ^a   Ishida, Kiyomichi ^a   Mizuno, Masahito ^a   Sumi, Takahiro ^a   Matsuzaki, Takashi ^b   Nagai, Junsei ^c   Murata, Hiroshi ^c  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b Institute of Space Technology and Aeronautics   (Japan)

^c Co Ltd   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

ATMOSPHERIC RE-ENTRY; CATALYTIC EFFECTS; ELECTRONIC EXCITATION TEMPERATURE; GAS SUPPLY SYSTEM; INDUCTIVELY-COUPLED; LOW MASS FLOW RATES; MAXIMUM HEAT FLUX; MAXIMUM POWER;

COMPUTATIONAL FLUID DYNAMICS; ELECTROMAGNETIC FIELDS; ENTHALPY; HEAT FLUX; INDUCTIVELY COUPLED PLASMA;

WIND TUNNELS;

EID: 84896741887     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (14)

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