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Titanium Aluminide Turbine Toolbox : Teilprojekt Access : Schlussbericht zum Verbundprojekt TATT
Ratcheting behavior of bearing support structures during windmilling in aero engines
State-Based Switching Control Strategy with Application to Aeroengine Safety Protection
Model-based temperature monitoring for broaching safety-critical aero engine components
Model-based temperature monitoring for broaching safety-critical aero engine components
Model-based temperature monitoring for broaching safety-critical aero engine components
Fortschrittliche Methoden zur Analyse von Wellenbruchszenarien bei Flugzeugtriebwerken
Melt-Infiltrated Refractory Ceramic Matrix Composites
The science, technology, and implementation of TiAl alloys in commercial aircraft engines
Non-destructive determination of local damage and material condition in high-performance components
Modern machining of advanced aerospace alloys - Enabler for quality and performance
Dynamic analysis of first stage compressor bladed disk of an aircraft engine
Application of the titanium alloy in civil aviation
Introducing new materials into aero engines - risks and rewards, a user's perspective
Schallemissionsprüfung zur Untersuchung der Langzeitschädigung von Brennkammerschindeln
Entwicklung und Eigenschaften intermetallischer Titanaluminide für Flugzeugtriebwerke
Entwicklung und Bewertung von Herstellungsprozessen für TiAl Verdichterschaufeln
Diffusion braze a NI-based single crystal alloy: Mechanical properties and microstructure
A comparison of nonlinear techniques for structural health monitoring
Vibration damping of aero engine rotors by elastomer ring bearings
Sprayforming optimisation of superalloy aeroengine components
HTS motors in aircraft propulsion: design considerations
Mechanical behavior of anti-symmetrically laminated composite blades
Herstellung und Eigenschaften von Superlegierungen mit zellularem Gefügeaufbau
Durability and fatigue cracks growth life of turbine blades of aircraft engine NK-8-2U
Thermal spray coatings: Broad and growing applications
Three-dimensional fatigue cracking under elastic-plastic deformation
Cast/wrought nickel-base superalloy designed for rotating components
Implications of engine's deterioration upon an aero-engine HP turbine blade's thermal fatigue life