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Flugtriebwerk
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A New Eulerian Model for Turbulent Evaporating Sprays in Recirculating Flows
Application of CFD in Combustor Design Technology
Calculs Aerothermochimiques dans les Foyers de Rechauffe
Combustion for Future Supersonic Transport Propulsion
Combustion Technology Needs for Advanced High Pressure Cycle Engines
Computational and Experimental Results in High Pressure Combustions of H~2/Air and H~2/O~2/H~2O
Design Aspects for Small Aircraft Gas Turbine Fuel Injectors
Effects of Hydrogen Addition on Pollutant Emissions in a Gas Turbine Combustor
Endothermic Fuels for Hypersonic Aviation
Evaluation of the Transient Operation of Advanced Gas Turbine Combustors
Experimental Studies on Effervescent Atomizers with Wide Spray Angles
Flowfield Prediction of NOx and Smoke Production in Aircraft Engines
Fuel Injector Design for High Temperature Aircraft Engine
High Temperature Fuel Requirements and Payoffs
Modelisation de la Phase Liquide dans les Chambres de Combustion
Numerical Modelling of Gas Turbine Combustion Chambers
Numerical Prediction of Turbulent Sooting Diffusion Flames
On the Effect of Emissions from Aircraft Engines on the State of the Atmosphere
Prediction of Prompt-NOx in Hydrocarbon Air Flames
Recent CFD Applications in Small Gas Turbine Combustion Systems Development
Reduction of NOx by Fuel-Staging in Gas Turbine Engines - A Commitment to the Future
Research and Development of High Thermal Stability Fuels
Simulation of Pollutant Formation in Turbulent Combustors Using an Extended Coherent Flame Model
Spray Combustion Experiments and Numerical Predictions
Studies of Lean Blowout in a Research Combustor
Technology Rigs - A Tool for Afterburner Development
The Mixing Process in the Quenching Zone of the Rich-Lean-Combustion Concept
Time-Resolved Measurements in a Three Dimensional Model Combustor
Ultra Low NOx Ultra Lean Gas Turbine Primary Zones with Liquid Fuels