Add to ORKGIgnition-delay distances for ethylene fuel injected into a supersonic combustor are modeled for jet-in-crossflow and shear-layer fuel-injection schemes using analytical models for entrainment and mixing, coupled with detailed chemical-kinetics simulations. Ignition delay distances are calculated for a two-dimensional parameter space of assumed vehicle flight Mach number and fuel-preheat stagnation temperature. The sensitivity of the ignition delays to these parameters is compared and discussed for the two fuel-injection schemes
Ethylene is a fuel considered for high-speed ram- and scramjet combustion applications, mainly becau...
Ethylene supersonic combustion flow field in different injection schemes was studied numerically in ...
Mixing and combustion of supersonic reacting flows are currently under investigation for new generat...
Ignition-delay distances for ethylene fuel injected into a supersonic combustor are modeled for jet-...
A computational analysis of ethylene combustion in scramjet engine applications has been performed. ...
Combustion in scramjet engines is faced with the limitation of brief residence time in the combustio...
Hydrocarbons become viable alternatives to hydrogen at Mach numbers below 10, because of greater fue...
Injecting fuel on the intake of scramjet engines is one strategy that might be used to minimize the ...
Multicomponent fuels, such as kerosene and diesel fuel, are the primary source of energy powering th...
Large Eddy Simulation (LES) and experiment were employed to investigate the transient ignition and f...
Numerical study of two dimensional supersonic hydrogen-air mixing layer is performed to investigate ...
An experimental and numerical investigation is performed to explore the methods for achieving flame ...
Single pulse shock tube facility has been developed in the High Temperature Chemical Kinetics Lab, A...
In this paper, supersonic combustion and flow field of hydrogen and its mixture with ethylene and me...
This paper considers the Eddy Dissipation Model to address the combustion process inside scramjet en...
Ethylene is a fuel considered for high-speed ram- and scramjet combustion applications, mainly becau...
Ethylene supersonic combustion flow field in different injection schemes was studied numerically in ...
Mixing and combustion of supersonic reacting flows are currently under investigation for new generat...
Ignition-delay distances for ethylene fuel injected into a supersonic combustor are modeled for jet-...
A computational analysis of ethylene combustion in scramjet engine applications has been performed. ...
Combustion in scramjet engines is faced with the limitation of brief residence time in the combustio...
Hydrocarbons become viable alternatives to hydrogen at Mach numbers below 10, because of greater fue...
Injecting fuel on the intake of scramjet engines is one strategy that might be used to minimize the ...
Multicomponent fuels, such as kerosene and diesel fuel, are the primary source of energy powering th...
Large Eddy Simulation (LES) and experiment were employed to investigate the transient ignition and f...
Numerical study of two dimensional supersonic hydrogen-air mixing layer is performed to investigate ...
An experimental and numerical investigation is performed to explore the methods for achieving flame ...
Single pulse shock tube facility has been developed in the High Temperature Chemical Kinetics Lab, A...
In this paper, supersonic combustion and flow field of hydrogen and its mixture with ethylene and me...
This paper considers the Eddy Dissipation Model to address the combustion process inside scramjet en...
Ethylene is a fuel considered for high-speed ram- and scramjet combustion applications, mainly becau...
Ethylene supersonic combustion flow field in different injection schemes was studied numerically in ...
Mixing and combustion of supersonic reacting flows are currently under investigation for new generat...
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