Supersonic combustion - A shock tunnel and vitiation-heated slowdown tunnel comparison

36th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1998, Pages

  Boyce, R R ^a   Wendt, M ^b   Paull, A ^a   Chinzei, N ^b   Stalker, R J ^a   Miyajima, H ^b  

^a UNIVERSITY OF QUEENSLAND   (Australia)

^b JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; BOUNDARY LAYERS; COMBUSTION; COMBUSTORS;

BOUNDARY LAYER GROWTH; COMBUSTOR GEOMETRY; EQUIVALENCE RATIOS; FREE-STREAM FLOW; HYDROGEN INJECTION; RECTANGULAR DUCTS; STATIC TEMPERATURE; SUPERSONIC COMBUSTION;

DUCTS;

EID: 84983103349     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (14)

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