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Volumn 33, Issue 2, 2011, Pages 2399-2405
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CFD analysis of the HyShot II scramjet combustor
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Author keywords
HyShot II wind tunnel experiments; Large Eddy Simulation; Scramjet; Self ignition; Supersonic mixing
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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;
AIR ENGINES;
ATMOSPHERIC BOUNDARY LAYER;
CHEMICAL ANALYSIS;
COMPUTER SIMULATION;
EXPERIMENTS;
IGNITION;
JET PUMPS;
LARGE EDDY SIMULATION;
MIXING;
NAVIER STOKES EQUATIONS;
RAMJET ENGINES;
WIND TUNNELS;
COMBUSTORS;
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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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References (27)
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