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Flugtriebwerk
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The science, technology, and implementation of TiAl alloys in commercial aircraft engines
Introducing new materials into aero engines - risks and rewards, a user's perspective
Ratcheting behavior of bearing support structures during windmilling in aero engines
The low temperature properties of aviation fuels
Durability and fatigue cracks growth life of turbine blades of aircraft engine NK-8-2U
Fiber-reinforced composites: the future for aeropropulsion
Crack growth modeling in an advanced powder metallurgy alloy
Keramischer Faserverbund statt metallischer Superlegierung
Entwicklung und Eigenschaften intermetallischer Titanaluminide für Flugzeugtriebwerke
Non-destructive determination of local damage and material condition in high-performance components
Dynamic analysis of first stage compressor bladed disk of an aircraft engine
Polymer, metal, and ceramic matrix composites for advanced aircraft engine applications
Design concepts for low cost composite engine frames
Wasserstoff-Metallhydride zur Speicherung und ein Flugzeug, das fliegt: Geballte Energieladung
Sprayforming optimisation of superalloy aeroengine components
Materials and process directions for advanced aero-engine design
Study of the propagation of kerosene explosions inside a partitioned vessel
Low area ratio aircraft fuel jet-pump performances with and without cavitation
Implications of engine's deterioration upon an aero-engine HP turbine blade's thermal fatigue life
Repair of air-cooled turbine vanes of high-performance aircraft engines. Problems and experience
The use of Kevlar on aero-engine fan containment casings
Modern machining of advanced aerospace alloys - Enabler for quality and performance
Three-dimensional fatigue cracking under elastic-plastic deformation
Design of hot ring rolling process using finite element analysis
HTS motors in aircraft propulsion: design considerations
Reducing Communication Overhead in Large Eddy Simulation of Jet Engine Noise
F-22 Raptor: Air dominance for the 21st century
Elektromagnetische Verfahren zum Nachweis von Wolframkarbideinschlüssen in Flugtriebwerksrotoren
Impact of engine cycle parameters on V/STOL type A configuration and commonality
Vorn mit Titan. Die britische Flugzeugindustrie schöpft aus dem Potential der Nachkriegszeit
Assessing halon alternatives for aircraft engine nacelle fire suppression
Diffusion braze a NI-based single crystal alloy: Mechanical properties and microstructure
Ceramic applications in turbine engines (CATE) program summary