Keywords: احتراق فوق العاده; Scramjet engine; Incomplete combustion; Supersonic combustion; Preliminary design;
مقالات ISI احتراق فوق العاده (ترجمه نشده)
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Keywords: احتراق فوق العاده; Detached eddy simulation; Reduced kinetic mechanism; Supersonic combustion; Hydrogen; Hydrocarbon;
Keywords: احتراق فوق العاده; Tabulated dynamic adaptive chemistry; Skeletal mechanism; Supersonic combustion; Ethylene; Large Eddy Simulation;
Keywords: احتراق فوق العاده; Supersonic combustion; k-É model; Double cavity combustor; Scramjet;
Keywords: احتراق فوق العاده; Flame stability; Supersonic combustion; DDT; Numerical simulations;
Keywords: احتراق فوق العاده; Combined solid fuel scramjet; Secondary combustion; Regression rate; Supersonic combustion;
Keywords: احتراق فوق العاده; Shock train; Numerical simulation; Heat release; Supersonic combustion;
Simulations of combustion oscillation and flame dynamics in a strut-based supersonic combustor
Keywords: احتراق فوق العاده; Large eddy simulation; Supersonic combustion; Pressure oscillation; Flame dynamic; Flame stabilization;
Effect of variation of hydrogen injection pressure and inlet air temperature on the flow-field of a typical double cavity scramjet combustor
Keywords: احتراق فوق العاده; Scramjet; Double cavity combustor; K-É model; Supersonic combustion;
Large eddy simulation of reacting flow in a hydrogen jet into supersonic cross-flow combustor with an inlet compression ramp
Keywords: احتراق فوق العاده; Large eddy simulation; Turbulent combustion; Hydrogen jet in supersonic cross-flow; Supersonic combustion; Flame structure;
Flame stabilization mechanism study in a hydrogen-fueled model supersonic combustor under different air inflow conditions
Keywords: احتراق فوق العاده; Flame stabilization; Large eddy simulation; Supersonic combustion; Hydrogen; Time scale comparison;
Effects of plate vibration on the mixing and combustion of transverse hydrogen injection for scramjet
Keywords: احتراق فوق العاده; Transverse injection; Vibration; Supersonic combustion; Mixing efficiency; Combustion efficiency; Combustion stability;
Keywords: احتراق فوق العاده; Large-eddy simulations; Supersonic combustion; Lifted jet flame; Shock wave;
Keywords: احتراق فوق العاده; Turbulent combustion; High-speed flow; Supersonic combustion; Distributed reaction; Computational fluid dynamics;
Keywords: احتراق فوق العاده; Supersonic combustion; Wall function boundary condition; Skin friction; Heat transfer; Numerical simulation
Keywords: احتراق فوق العاده; Hydrogen; Scramjet; Supersonic combustion; Oblique shock;
Keywords: احتراق فوق العاده; Ignition transients; Supersonic combustion; Large eddy simulation; Dual-cavity;
Keywords: احتراق فوق العاده; Hydrogen combustion; Flame acceleration; Chocked flame; Supersonic combustion; Deflagration-to-detonation transition; Detonation;
Keywords: احتراق فوق العاده; Supersonic combustion; Large-eddy simulation;
Keywords: احتراق فوق العاده; CFD; Scramjet; Combustion efficiency; SST k-ω model; Supersonic combustion; Angle of attack
Keywords: احتراق فوق العاده; Supersonic combustion; Laminar finite rate model; Flamelet model; Numerical simulation
Keywords: احتراق فوق العاده; Detonation; Rotating detonation combustor; Supersonic combustion; Pressure feedback; Resonance;
Keywords: احتراق فوق العاده; Large eddy simulation; Passive scalar; Supersonic combustion; Cavity
Keywords: احتراق فوق العاده; Hydrogen; Supersonic combustion; Flamelet/progress variable model; Improved delayed detached eddy simulation;
Keywords: احتراق فوق العاده; Large eddy simulation; Scramjet; Dual cavity; Supersonic combustion
Keywords: احتراق فوق العاده; Supersonic combustion; Plasma assistance; Combustion instability
Keywords: احتراق فوق العاده; Supersonic combustion; Scramjet; Shock train; Ground testing
Keywords: احتراق فوق العاده; Rotating detonation; Instability; RDE; Combustor; Supersonic combustion;
Keywords: احتراق فوق العاده; Supersonic combustion; Shock and combustion interactions; Transverse injection; Compressibility modification
Keywords: احتراق فوق العاده; Scramjet; Large eddy simulation; Supersonic combustion; Flamelet
Keywords: احتراق فوق العاده; Large eddy simulation; Supersonic combustion; Dual-cavity; Flame structure
Keywords: احتراق فوق العاده; Turbulent combustion; Compressible flow; Supersonic combustion; Scramjet; Flamelet
Keywords: احتراق فوق العاده; Supersonic combustion; Scramjets; Large-eddy simulation; Cavity flameholder; Ethylene combustion
Keywords: احتراق فوق العاده; Aeroengine; Control; Modeling; Scramjet engine; Supersonic combustion
Keywords: احتراق فوق العاده; Supersonic combustion; Combustion instabilities; Ramps; Cavities; Mixing
Keywords: احتراق فوق العاده; Graphite combustion; High temperature combustion; Supersonic combustion
Keywords: احتراق فوق العاده; Partially premixed; Multi-regime flamelet model; Hydrogen; Supersonic combustion; Combustion regime index;
Keywords: احتراق فوق العاده; Solid fuel scramjet; Cavity structure; Shock waves; Supersonic combustion;
Intermittent back-flash phenomenon of supersonic combustion in the staged-strut scramjet engine
Keywords: احتراق فوق العاده; Flame propagation; Back flash; Supersonic combustion; Staged-strut scramjet;
Hybrid RANS/LES of a supersonic combustor
Keywords: احتراق فوق العاده; Hybrid RANS/LES; URANS; Supersonic combustion; Finite-rate chemistry; Scramjet; Combustion simulation;
From ignition to stable combustion in a cavity flameholder studied via 3D tomographic chemiluminescence at 20Â kHz
Keywords: احتراق فوق العاده; 3D measurements; Tomography; Fiber based endoscopes; Supersonic combustion;
Analysis of flame characteristics in a scramjet combustor with staged fuel injection using common path focusing schlieren and flame visualization
Keywords: احتراق فوق العاده; Flame stabilization and structures; Focusing schlieren imaging; Dual-mode scramjet; Supersonic combustion; Strut injection;
Effects of thermally cracked component of n-dodecane on supersonic combustion behaviors in a scramjet model combustor
Keywords: احتراق فوق العاده; Supersonic combustion; Hydrocarbon fuels; Thermal cracking; Scramjet;
Ignition characteristics of laser-ionized fuel injected into a hypersonic crossflow
Keywords: احتراق فوق العاده; Supersonic combustion; Laser-induced ignition; Scramjets; Plasma-assisted combustion; Laser-induced plasma; Laser-ionized fuel
Numerical investigation on hydrogen combustion in a scramjet with 3D sidewall compression inlet
Keywords: احتراق فوق العاده; Supersonic combustion; Inlet distortion; Sidewall compression inlet; CFD
DNS analysis of a three-dimensional supersonic turbulent lifted jet flame
Keywords: احتراق فوق العاده; Direct numerical simulation; Supersonic combustion; Compressibility; Premixed flame; Diffusion flame;
Laser-induced plasma ignition studies in a model scramjet engine
Keywords: احتراق فوق العاده; Hypersonic flow; Supersonic combustion; Planar laser-induced fluorescence imaging; Plasma-assisted combustion; Laser-induced ignition; Laser-induced plasma
Ignition delay time in swirling supersonic flow
Keywords: احتراق فوق العاده; Ignition delay; Supersonic combustion; Swirl; Numerical simulation; Turbulence
A computational study of the HyShot II combustor performance
Keywords: احتراق فوق العاده; Scramjet; HyShot II wind-tunnel and flight experiments; Large Eddy Simulation; Supersonic combustion; Modes of operation
Combustion characteristics in a supersonic combustor with hydrogen injection upstream of cavity flameholder
Keywords: احتراق فوق العاده; Cavity flameholder; Supersonic combustion; Flameholding