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Oxidation behaviour of MIM-processed Nickel based superalloys
New manufacturing techniques for new engine component design
Materials for competitive aero engines
The future of aero engines and the requirements for instrumentation and measurement technologies
Dealing with a complex Teamcenter environment in the aero engines industry - practical experiences
Eco-efficient aero engines - short, medium and long-term concepts
Cyclic mixed-mode crack propagation due to time-dependent multiaxial loading in jet engines
Effects of the surface treatment on the measured diffraction peak width of Inconel 718
Ultrasonic Shot Peening (USP) for Ti-6AI-4V and Ti-6AI-2Sn-4Zr-6Mo aero engine components
Sage4 Geared Turbofan demonstrator
Finite element modeling of porous nickel base cast alloys with representative volume elements
Adaptive technologies in repair processes for aero engines
Measurement of 2D dynamic stress distributions with a 3D-scanning laser poppler vibrometer
State of the art technology for aero engines and for IGTs
NEWAC - A European technology program
Air Breathing Propulsion - Quo vadis?
Application of crystal temperature sensors in engine testing
A microstructural finite element model for Ni-base cast alloys
Modelling of roughness-induced transition using local variables
Rayleigh wave velocity dispersion for characterization of surface treated aero engine alloys
Overview of the NEWAC-Programme
Propagation of cracks in selected subject to mixed-mode
The Geared Turbofan - Turning the technology into next generation of fuel efficient engines
The future of EB-PVD TBCs - operational side and potentials for further improvemente´s
Newac subproject 2 "Intercooled recuperative core" - editorial
Magnetic bearings for smart aero engines
Basic Principles – Gas Turbine Compatibility – Intake Aerodynamic Aspects
Basic Principles – Gas Turbine Compatibility – Gas Turbine Aspects
CLAIRE - MTU Clean Air Engine Program
Blisk Production of the Future
Evaluation of mixed-mode cyclic crack propagation in aero engine structures
Surface measurement of dynamic stress distribution on turbine blades
Coatings for advanced aero engine materials
Powerful Pace-Setter in Turbomachinery Development
Near-surface residual stress-profiling with high frequency eddy current conductivity measurement
PLM harmonization as a strategic asset for effective NPI processes
SiC long fibre reinforced copper for the divertor heat sink
Out of plane crack growth using the mixed element approach
Optimal probe arrangement for ultrasonic inspection of spin test disks
Application of the Zienkiewicz-Zhu error estimator in aero engines
Retrofit of a digital engine control unit and integration of an active stability control system
GP7000: MTU Aero Engines` contribution in a successful partnership
Phases of high-tech repair implementation
The Geared Turbofan technology - opportunities, challenges and readiness status
Total temperature probes for turbine and combustor applications
Advanced technologies for next generation regional jets
Aero Engine material requirements, compositions, processing, properties, applications
Automatic mixed-mode crack propagation based on a combined hexahedral-tetrahedral approach
Using automated data quality check tools - lifecycle-oriented product data management, Part 1
Using automated data quality check tools - lifecycle-oriented product data management, Part 2
Recent titanium research and development in Germany
MTU solutions against erosive attack and loss of EGT margin in turbo engines - ERCoatnt
Cooperating twin robots form a new X-ray diffractometer for stress analysis
Flow control in turbomachinery using micro jets
Modeling attempts to predict fretting-fatigue life on turbine components
Thermomechanical design of a heat exchanger for a recuperative aero engine
Crack detection using EddyTherm
Towards collaborative engineering in the aerospace industry
The engine industry - new avenues to A new century
Guideline for direct part marketing of aero engine parts
Preliminary gas turbine design using the multidisciplinary design system MOPEDS
Assessment of failure mechanisms of aero engine TMC rotor disks at high rates of strain
Investigations into engine transient response due to internal and external dynamic excitations