Synonyms were used for:
Flugtriebwerk
Search without synonyms:
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
Smart Flow Control in Aircraft Engine Components & Component Interactions
Simultaneous Active Source Control of Blade Row Interaction Generated Discrete Tones
Simulation of Pollutant Formation in Turbulent Combustors Using an Extended Coherent Flame Model
Simulation of Crack Propagation in Engine Rotating Components Under Variable Amplitude Loading
Rotating Pip Detection and Stall Warning in High-Speed Compressors Using Structure Function
Research and Development of High Thermal Stability Fuels
Reduction of NOx by Fuel-Staging in Gas Turbine Engines - A Commitment to the Future
Recent CFD Applications in Small Gas Turbine Combustion Systems Development
Process Optimization in Advanced Compressor Design
Prediction of Prompt-NOx in Hydrocarbon Air Flames
Part Speed Flutter of Transonic Fans
On the Effect of Emissions from Aircraft Engines on the State of the Atmosphere
Numerical Simulation of Multi-Stage Turbomachinery Flows
Numerical Prediction of Turbulent Sooting Diffusion Flames
Numerical Modelling of Gas Turbine Combustion Chambers
Monitoring and Control of Helicopter Engines at Abnormal Operating Conditions
Modelisation de la Phase Liquide dans les Chambres de Combustion
La fiabilite des roulements aeronautiques et le comportement en fatigue
Keynote Address "Design Principles and Methods for Military Turbojet Engines"
Improved Gas Turbine Response using LQR Control
High Temperature Fuel Requirements and Payoffs
Fuel/Oil System Thermal Management in Aircraft Turbine Engines
Fuel Injector Design for High Temperature Aircraft Engine
Forced Response Predictions for a HP Turbine Rotor Blade