Comparison of supersonic combustion between impulse and vitiation-heated facilities

Journal of Propulsion and Power

Volumn 16, Issue 4, 2000, Pages 709-717

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

^a IMPERIAL COLLEGE LONDON   (United Kingdom)

^b UNIVERSITY OF QUEENSLAND   (Australia)

^c JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^d Centre for Dynamics   (United States)

^e KAKUDA RESEARCH CENTER   (Japan)

^f CSIRO   (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; COMBUSTION; STREAM FLOW; SUPERSONIC FLOW;

SCRAMJETS; SUPERSONIC COMBUSTION;

AIRCRAFT PROPULSION;

EID: 0034224719     PISSN: 07484658     EISSN: None     Source Type: None    
DOI: 10.2514/2.5631     Document Type: Article

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