Journal of Propulsion and Power · 2011 · 34 citations · 25 references
EngineeringChemical EngineeringMechanical EngineeringCombustionHeat TransferReaction EngineeringCombustion FundamentalsCombustion KineticsCombustion ProcessesCombustion ThermodynamicsGas Turbine CombustionGas Turbine EnginesCombustion CharacteristicsCombustion-related Nitrogen OxidesCombustor AerodynamicsCombustor DesignFlame DiagnosticsFlame SpeedFlame Structure AnalysisNozzle Analysis
Nomenclature d = inner diameter of the FLOX® nozzle, mm Da = Damkohler number dl = position of fuel nozzle with respect to air nozzle exit plane, mm f = focal length, mm k = rate coefficient NOx = oxides of nitrogen (NO and NO2) OH = OH chemiluminescence (electronically excited) Tad = global adiabatic flame temperature, K Tair = air preheat temperature, K v = velocity in air nozzle, ms 1 = air equivalence ratio = equivalence ratio
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Antonio Cavaliere, Mara de Joannon · Progress in Energy and Combustion Science · 2004 · 1.2K citations