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Flugtriebwerk
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Aircraft Engine Historical Society
Structural design of aircraft engines : key objectives and techniques
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
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
Simultaneous Active Source Control of Blade Row Interaction Generated Discrete Tones
La fiabilite des roulements aeronautiques et le comportement en fatigue
Keynote Address "Design Principles and Methods for Military Turbojet Engines"
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
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
Theory for the Use of Foreign Gas in Simulating Film Cooling