Add to ORKGA simple flow/thermodynamic model is proposed to describe finite chemical kinetic rate combustion in a turbulent supersonic shear layer for the purposes of assessing Damköhler number effects in such flows. Sample calculations and comparisons for the H_2/NO/F_2 chemical system and the H_2/air system are described for a set of initial flow and thermodynamic conditions of the entrained reactants
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
The capability of empirical combustion models to predict the mean reaction rate for supersonic mixin...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
A simple flow/thermodynamic model is proposed to describe finite chemical kinetic rate combustion ...
The physical phenomena involved when a supersonic flow undergoes chemical reaction are discussed. De...
A model is proposed for calculating molecular mixing and chemical reactions in fully developed turbu...
A model is proposed for calculating molecular mixing and chemical reactions in fully developed turbu...
Work is continuing primarily in gas phase turbulent mixing and chemical reactions. The liquid phase ...
This is a continuing effort in both gas phase and liquid phase mixing, chemical reactions and combus...
This is a continuing effort in both gas phase and liquid phase mixing, chemical reactions and combus...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
The physical phenomena within supersonic flows that sustain chemical reactions are investigated. An ...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
The capability of empirical combustion models to predict the mean reaction rate for supersonic mixin...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
A simple flow/thermodynamic model is proposed to describe finite chemical kinetic rate combustion ...
The physical phenomena involved when a supersonic flow undergoes chemical reaction are discussed. De...
A model is proposed for calculating molecular mixing and chemical reactions in fully developed turbu...
A model is proposed for calculating molecular mixing and chemical reactions in fully developed turbu...
Work is continuing primarily in gas phase turbulent mixing and chemical reactions. The liquid phase ...
This is a continuing effort in both gas phase and liquid phase mixing, chemical reactions and combus...
This is a continuing effort in both gas phase and liquid phase mixing, chemical reactions and combus...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
The physical phenomena within supersonic flows that sustain chemical reactions are investigated. An ...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
The capability of empirical combustion models to predict the mean reaction rate for supersonic mixin...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...