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Flugtriebwerk
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keywords:(Flugtriebwerk)
Fuel Injector Design for High Temperature Aircraft Engine
Flowfield Prediction of NOx and Smoke Production in Aircraft Engines
Time-Resolved Measurements in a Three Dimensional Model Combustor
A New Eulerian Model for Turbulent Evaporating Sprays in Recirculating Flows
Reduction of NOx by Fuel-Staging in Gas Turbine Engines - A Commitment to the Future
Technology Rigs - A Tool for Afterburner Development
Numerical Modelling of Gas Turbine Combustion Chambers
Numerical Prediction of Turbulent Sooting Diffusion Flames
Effects of Hydrogen Addition on Pollutant Emissions in a Gas Turbine Combustor
Design Aspects for Small Aircraft Gas Turbine Fuel Injectors
Recent CFD Applications in Small Gas Turbine Combustion Systems Development
Ultra Low NOx Ultra Lean Gas Turbine Primary Zones with Liquid Fuels
High Temperature Fuel Requirements and Payoffs
Prediction of Prompt-NOx in Hydrocarbon Air Flames
Computational and Experimental Results in High Pressure Combustions of H~2/Air and H~2/O~2/H~2O
Application of CFD in Combustor Design Technology
The Mixing Process in the Quenching Zone of the Rich-Lean-Combustion Concept
Studies of Lean Blowout in a Research Combustor