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Volumn 219, Issue 3, 2005, Pages 205-216

Numerical investigation of transverse sonic injection in a non-reacting supersonic combustor

Author keywords

Backward facing step; Dynamic pressure ratio; Scramjet; Transverse injection

Indexed keywords

COMBUSTION; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; COMPUTER SOFTWARE; FUELING; HEAT LOSSES; JET AIRCRAFT; NAVIER STOKES EQUATIONS; TURBULENCE;

EID: 24344493903     PISSN: 09544100     EISSN: None     Source Type: Journal    
DOI: 10.1243/095441005X30261     Document Type: Conference Paper
Times cited : (27)

References (22)
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.