Keywords: مشعل توربین گاز; Gas turbine combustor; Low emissions; Lean direct injection; Airblast injector; Swirl-venturi configuration;
مقالات ISI مشعل توربین گاز (ترجمه نشده)
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Keywords: مشعل توربین گاز; Flame stability; Gas turbine combustor; Hydrogen enrichment; Oxy-combustion; Swirl effect;
Keywords: مشعل توربین گاز; Gas turbine combustor; Fuel concentration; Liquid fuel; Combustion; Trapped vortex combustor; Droplet;
Keywords: مشعل توربین گاز; Oxy-combustion; Oxygen-enriched air combustion; Non-premixed flames; Stability maps; Flammability limits; Gas turbine combustor;
Keywords: مشعل توربین گاز; Gas turbine combustor; Swirl flows; Proper orthogonal decomposition; Combustor turbulence; Combustor coherent structures; Precessing vortex core;
Keywords: مشعل توربین گاز; Gas turbine combustor; Steam addition; Preliminary combustor design; Performance
Keywords: مشعل توربین گاز; Gas turbine combustor; Combustion instability; Synthetic natural gas; Proper orthogonal decomposition; High-speed OH chemiluminescence;
Keywords: مشعل توربین گاز; Swirling flow; Vortex breakdown; Gas turbine combustor; Outlet contraction
Keywords: مشعل توربین گاز; Large-eddy simulation; Gas turbine combustor; Turbulence/chemistry interaction; Flamelet modeling; Turbulent combustion;
Keywords: مشعل توربین گاز; Gas turbine combustor; Inflow boundary condition generation methods; Large-eddy simulation (LES); Sub-grid scale (SGS) model; Turbulent flows
Keywords: مشعل توربین گاز; Gas turbine combustor; Combustion instabilities; Vortex breakdown; Swirling flows; High speed diagnostics; SPIV
Keywords: مشعل توربین گاز; Numerical simulation of turbulent combustion; Oxy-fuel; Syngas; Gas Turbine Combustor;
Keywords: مشعل توربین گاز; Swirling flow; Swirler; Design methodology; Gas turbine combustor; Combustion chamber
Keywords: مشعل توربین گاز; Gas turbine combustor; Oxy-combustion; Oxygen permeation; ITM reactor
Keywords: مشعل توربین گاز; High pressure combustion; Gas turbine combustor; Turbulent premixed swirl flame; Raman scattering; Particle image velocimetry; Turbulence-chemistry interaction;
Numerical analysis of a gas turbine combustor fueled by hydrogen in comparison with jet-A fuel
Keywords: مشعل توربین گاز; Combustion; Hydrogen; Gas turbine combustor; CFD;
Comparative study of non-premixed and partially-premixed combustion simulations in a realistic Tay model combustor
Keywords: مشعل توربین گاز; CFD; Combustion modelling; Gas turbine combustor; Non-premixed flame; Partially-premixed flame;
Design of a multi-can carbon-free gas turbine combustor utilizing multiple shell-and-tube OTRs for ZEPP applications
Keywords: مشعل توربین گاز; Oxygen transport reactor (OTR); Gas turbine combustor; Carbon-free; Oxygen permeation; Oxy-fuel combustion; Zero emission power plant (ZEPP);
Effects of nitrogen dilution on the NOx and CO emission of H2/CO/CH4 syngases in a partially-premixed gas turbine model combustor
Keywords: مشعل توربین گاز; Gas turbine combustor; NOx and CO emission; Synthetic gas; Nitrogen dilution; OH∗ chemiluminescence; Flame stability
Coupling of flame geometry and combustion instabilities based on kilohertz formaldehyde PLIF measurements
Keywords: مشعل توربین گاز; Instability; Dimethyl ether; Formaldehyde PLIF; High-speed; Gas turbine combustor;
Combustion characteristics of a slotted swirl combustor: An experimental test and numerical validation
Keywords: مشعل توربین گاز; Slotted swirler; Gas turbine combustor; Non-premixed combustion; Central recirculation zone
Experimental and numerical investigation of Helmholtz resonators and perforated liners as attenuation devices in industrial gas turbine combustors
Keywords: مشعل توربین گاز; Combustion instability; Gas turbine combustor; Helmholtz resonator; Perforated liner; CFD
CO2 radiation heat loss effects on NOx emissions and combustion instabilities in lean premixed flames
Keywords: مشعل توربین گاز; Gas turbine combustor; Combustion instability; CO2; Lean premixed combustion; Radiation heat transfer;
Effect of fuel-air mixture velocity on combustion instability of a model gas turbine combustor
Keywords: مشعل توربین گاز; Flame structure; Fluid dynamic instability; Combustion dynamics; OH* chemiluminescence; Gas turbine combustor;
Effects of unstable flame structure and recirculation zones in a swirl-stabilized dump combustor
Keywords: مشعل توربین گاز; Gas turbine combustor; Combustion dynamics; Flame vortex structure; OH chemiluminescence; Particle image velocimetry (PIV); Central recirculation zone (CRZ);
Numerical investigation of the flow and flame structure in an axisymmetric trapped vortex combustor
Keywords: مشعل توربین گاز; Trapped vortex; Gas turbine combustor; Momentum flux ratio; Flame structure;
Spark ignition of turbulent recirculating non-premixed gas and spray flames: A model for predicting ignition probability
Keywords: مشعل توربین گاز; 20.020; 70.050; 80.010; 70.070Spray; Spark ignition; Gas turbine combustor; Turbulent combustion
Wide band correlated-k approaches for non-grey radiation modelling in oxy-fuel combustion with dry recycling
Keywords: مشعل توربین گاز; Radiative heat transfer; Spectral modelling; Wide band correlated-k method; Oxy-fuel combustion; Gas turbine combustor
Real-time equivalence ratio measurements in gas turbine combustors with a near-infrared diode laser sensor
Keywords: مشعل توربین گاز; Diode laser; Wavelength modulation spectroscopy; Equivalence ratio measurement; Gas turbine combustor
A study of jet fuel sooting tendency using the threshold sooting index (TSI) model
Keywords: مشعل توربین گاز; Jet fuel; Gas turbine combustor; Soot; Fuel composition; Sooting tendency; Hydrogen content; Smoke point
LES studies of the flow in a swirl gas combustor
Keywords: مشعل توربین گاز; Large eddy simulation; Premixed swirling flame; Gas turbine combustor