Add to ORKGThe research for developing a modular computer program for describing gas-turbine combustor flow and chemical fields is reported. The status of investigations is presented for three key elements of the unified model: turbulent mixing with swirl, turbulent mixing with swirl including finite-rate kinetics, and multiphase recirculation zone analysi
De nos jours, la combustion d'hydrocarbures est largement répandue dans de nombreuses applications, ...
The notion of "global warming" has become a major public-domain concept as an environmental threat t...
Mini turbojet engines can be widely used for unmanned aerial vehicles due to their main advantages o...
Research on combustion is being conducted at Lewis Research Center to provide improved analytical mo...
A model which predicts nitric oxide and carbon monoxide emissions from a swirl can modular combustor...
The flowfields of gas turbine combustion chambers were investigated. Six flowfield configurations wi...
Research on combustion is being conducted to provide improved analytical models of the complex flow ...
Fluid mechanical effects on combustion processes in steady flow combustors, especially gas turbine c...
This report includes copies of relevant publications, including conference proceedings, resulting fr...
The objectives of this program are to establish an experimental data base documenting the behavior o...
Aerothermal submodels used in analytical combustor models are analyzed. The models described include...
The overall objective of the Turbine Engine Hot Section Technology Combustion Project was to develop...
Gas emissions were studied from a staged Rich Burn/Quick-Quench Mix/Lean Burn combustor were studied...
The goal of this research is to bring computational fluid dynamics to a state of practical applicati...
The Turbine Engine Hot Section Technology Combustion Program is briefly described. The overall objec...
De nos jours, la combustion d'hydrocarbures est largement répandue dans de nombreuses applications, ...
The notion of "global warming" has become a major public-domain concept as an environmental threat t...
Mini turbojet engines can be widely used for unmanned aerial vehicles due to their main advantages o...
Research on combustion is being conducted at Lewis Research Center to provide improved analytical mo...
A model which predicts nitric oxide and carbon monoxide emissions from a swirl can modular combustor...
The flowfields of gas turbine combustion chambers were investigated. Six flowfield configurations wi...
Research on combustion is being conducted to provide improved analytical models of the complex flow ...
Fluid mechanical effects on combustion processes in steady flow combustors, especially gas turbine c...
This report includes copies of relevant publications, including conference proceedings, resulting fr...
The objectives of this program are to establish an experimental data base documenting the behavior o...
Aerothermal submodels used in analytical combustor models are analyzed. The models described include...
The overall objective of the Turbine Engine Hot Section Technology Combustion Project was to develop...
Gas emissions were studied from a staged Rich Burn/Quick-Quench Mix/Lean Burn combustor were studied...
The goal of this research is to bring computational fluid dynamics to a state of practical applicati...
The Turbine Engine Hot Section Technology Combustion Program is briefly described. The overall objec...
De nos jours, la combustion d'hydrocarbures est largement répandue dans de nombreuses applications, ...
The notion of "global warming" has become a major public-domain concept as an environmental threat t...
Mini turbojet engines can be widely used for unmanned aerial vehicles due to their main advantages o...