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Flugtriebwerk
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Aircraft Engine Historical Society
Structural design of aircraft engines : key objectives and techniques
Simultaneous Active Source Control of Blade Row Interaction Generated Discrete Tones
La fiabilite des roulements aeronautiques et le comportement en fatigue
Advanced CFD Tools for Multi-Stage Turbine Analysis
Afterburner Design and Development
Fault Tolerant Design Methodology in Software for Safety Related Systems
Computer Modeling of Heat Generation in Vapor Lubricated Bearings for Gas Turbines
The PW100 Engine: 20 Years of Gas Turbine Technology Evolution
The Potential of Advanced Materials on Structural Design of Future Aircraft Engines
Design of an Active Stall Avoidance System for a Subsonic Axial Compressor
Improved Gas Turbine Response using LQR Control
Fuel/Oil System Thermal Management in Aircraft Turbine Engines
F/A-18 E/F Aircraft Engine (F414-GE-400) Design and Development Methodology
Design of a New Fighter Engine - The Dream in an Engine Man's Life
Design Principles for the Quench Zone of Rich-Quench-Lean Combustors
Advanced Seal Technology Role in Meeting Next Generation Turbine Engine Goals
Process Optimization in Advanced Compressor Design
Smart Flow Control in Aircraft Engine Components & Component Interactions
Simulation of Crack Propagation in Engine Rotating Components Under Variable Amplitude Loading
A Mixed Flow Turbofan Afterburner Simulation for the Definition of Reheat Fuel Control Laws
The Benefits of a Rotating Rig for Research into Advanced Turbine Cooling Systems
Rotating Pip Detection and Stall Warning in High-Speed Compressors Using Structure Function
Cycle-Match Engine Models used in Functional Engine Design - An Overview
Part Speed Flutter of Transonic Fans
A One Dimensional, Time Dependent Inlet/Engine Numerical Simulation for Aircraft Propulsion Systems
Monitoring and Control of Helicopter Engines at Abnormal Operating Conditions
Actuation System for Variable Exhaust Nozzle and Inlet Guide Vanes on an Advanced Gas Turbine Engine
Keynote Address "Design Principles and Methods for Military Turbojet Engines"
Forced Response Predictions for a HP Turbine Rotor Blade
Turbomachinery Blade Design Using a Navier-Stokes Solver and Artificial Neural Network
Three-Dimensional Inverse Design Method for Turbine and Compressor Blades
Theory for the Use of Foreign Gas in Simulating Film Cooling
Advanced Computational Fluid Dynamics in the Design of Military Turbines
Numerical Simulation of Multi-Stage Turbomachinery Flows
The Gas Turbine Engine Conceptual Design Process - An Integrated Approach
Aero-Thermo-Structural Design Optimization of Internally Cooled Turbine Blades
The Introduction of Reinforced TMC Materials into Rotating Machinery - The Safe Approach
Designing for Reliability - The Rolls-Royce Approach
Evaluation of the Transient Operation of Advanced Gas Turbine Combustors
Simulation of Pollutant Formation in Turbulent Combustors Using an Extended Coherent Flame Model
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