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Volumn 33, Issue 2, 2011, Pages 2399-2405

CFD analysis of the HyShot II scramjet combustor

Author keywords

HyShot II wind tunnel experiments; Large Eddy Simulation; Scramjet; Self ignition; Supersonic mixing

Indexed keywords

AIR BREATHING ENGINES; CFD ANALYSIS; COMBUSTION EFFICIENCIES; COMBUSTION PRO-CESS; COMPLICATED FLOW; CROSS FLOWS; EXPERIMENTAL DATA; HEAT RELEASE; HIGH ENTHALPY SHOCK TUNNEL; INFLOW BOUNDARY CONDITIONS; JET PENETRATION; LARGE EDDY SIMULATION MODELS; MIXING ZONES; PRESSURE RISE; RAMJETS; REACTING FLOWS; REDUCED CHEMISTRY; REYNOLDS-AVERAGED NAVIER-STOKES; SCRAMJET; SCRAMJET COMBUSTORS; SCRAMJET ENGINES; SELF-IGNITION; SUPERSONIC COMBUSTION; SUPERSONIC MIXING; TURBULENT COMBUSTION; TURBULENT MIXING; VOLUMETRIC EXPANSION; WALL PRESSURE; WIND TUNNEL EXPERIMENT;

EID: 79251618337     PISSN: 15407489     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.proci.2010.07.055     Document Type: Article
Times cited : (101)

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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.