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Flugtriebwerk
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keywords:(Flugtriebwerk)
Ultra Low NOx Ultra Lean Gas Turbine Primary Zones with Liquid Fuels
Turbomachinery Blade Design Using a Navier-Stokes Solver and Artificial Neural Network
Time-Resolved Measurements in a Three Dimensional Model Combustor
Three-Dimensional Inverse Design Method for Turbine and Compressor Blades
The PW100 Engine: 20 Years of Gas Turbine Technology Evolution
The Potential of Advanced Materials on Structural Design of Future Aircraft Engines
Theory for the Use of Foreign Gas in Simulating Film Cooling
The Mixing Process in the Quenching Zone of the Rich-Lean-Combustion Concept
The Introduction of Reinforced TMC Materials into Rotating Machinery - The Safe Approach
The Gas Turbine Engine Conceptual Design Process - An Integrated Approach
The Benefits of a Rotating Rig for Research into Advanced Turbine Cooling Systems
Technology Rigs - A Tool for Afterburner Development
Studies of Lean Blowout in a Research Combustor
Structural design of aircraft engines : key objectives and techniques
Spray Combustion Experiments and Numerical Predictions