PrintDevelopment
Basics
Towards the Powerhouse for More Electric Aircraft - Dedicated Engine Concepts
Automatic cyclic crack propagation calculations in aircraft engines
Heat and fluid flow investigations on a heat exchanger for aero engine application
Rotordynamics and uncertainty of variables
Opportunities and challenges for more intelligent gas turbine engines
Spoke centering eccentricity-statistical tolerance analysis
Collaborative multi-company- multi-disciplinary jet engine design optimazation
Active core technology within the newac research program for cleaner and more efficient aero engines
New environmental friendly aero engine core concepts
Ideal workflow and process planning concept for the product development phase
Development of air seal system for modern jet engines
Temperature gradients in TMF specimes measurement and influence on TMF life
Clean validation of the Geared Turbofan high speed turbine integration of heat exchanger technique
Cyclic crack propagation calculations in an industrial environment
CLEAN-bench adaption and test for a complex demo engine concept
Noncontact blade vibration measurement system for aero engine application
Sensor checking using model based engine performance test
Multiple stage turbofan bird ingestion analysis
Constitutive equations in finite element codes
Modelling route for abradable coatings
Mixed-mode crack propagation calculations in a pure hexahedral mesh
Process optimization, innovative work environment for concurrent engineering
Intercooled recuperated aero engine
Non-linearities in an Aaero engine structure: from test to design
Numerical investigation of blade flutter at or near stall in axial flow turbomachines
Algorithmic aero engine life usage monitoring based on reference analysis of design mission
Experiments in active stall control of a twin-spool turbofan engine
Model based control concepts for jet engines
The use of onboard real-time models for jet engine control
Validation of a mixed flow turbofan performance model in the sub-idle operating range
Realtime capability for an off-the-shelf full thermodynamic engine performance computer program
Advanced propulsion system simulation model for a modern fighter aircraft training
Design features and procedures to reduce the phenomenon of HP-rotor bow on jet engines
Innovative processes for collaborative engineering in the aero engine industry
Achieving maximum thermal efficiency with the simple gas turbine cycle
Supporting distributed engineering in the aerospace industry
Compressors
FRAP measurements at a stability enhanced high pressure compressor
Design and analysis of the transonic flutter research compressor Fanny
Reliability of time-linearized flutter predictions near the surge line
Controlled excitation of rotor blades via macro fiber composites in an axial compressor
Excitation of Rotor Blades via Macro Fiber Composites in an Axial Compressor
A parameter study on the influence of filletes in the compressor cascade performance
Compressor Rig Testing at MTU Aero Engines: Testbed / Instrumentation / Data Acquisition
Compressor Rig Testing at MTU Aero Engines: Model-Based Data Analysis
Damping of a compressor vane cluster
The effect of forward sweep in a transonic compressor rotor
Influence of sweep on the 3D shock structure in an axial transonic compressor
Impact of a fillet on diffusing vane endwall flow structure
ATFI-HDV: Design of a new 7 stage innovative compressor
Noncontact crack detection on compressor rotor blades
Compressor noise reduction with CFD blade design
Control of coating properties of abradable seals
Aerodynamic and mechanical vibration analysis of a compressor blisk
Low noise compressor design with a linearized Euler method
Advanced high temperature turbine seals materials and designs
Active stability control of the compression system
Impact of transonic compressor rotor leading edge
Computational investigation of an oscillating compressor cascade experiment
Design improvements of the EJ200 HP compressor
On the performance of compressor blades with contoured endwalls
Advanced compressor technology - key success factor for competitiveness in modern aero engines
Mistuning and coupling effects in turbomachinery bladings
Turbines
Validation of an integrated acoustic absorber in a turbine exit guide vade
Heat transfer and pressure drop characteristics for a turbine casing impingement cooling system
ACTRAN TM cross-validation cersus ACTRAN DGM: A 2D-numerical study
Einfluss der Mikrostruktur auf die mechanischen Eigenschaften einer Nb-reichen y-TiAl-Legierung
Sound generation of a turbine stage due to nonuniform mean flow temperatures
"Online Troughflow" - Automatic simultaneous simulation of an axial flow turbine
LP turbine reynolds lapse phenomena: time averaged area traverse and multistage cfd
Design and construction of a two shaft test turbine for investigation of mid turbine frame flows
Comparison between the flow through an aggressive and a super-aggressive intermediate turbine duct
Validation of turbine noise prediction tools with acoustic rig measurements
On Flow Separation in a super-aggressive intermediate turbine duct
LP turbine laminar separation bubble study, PIV results on flat plate and DNS comparison
A study of unsteady secondary flow in a water flow axial turbine model
Preparation of aero technology for new generation aircraft engine LP turbines
Numerical investigations for optimizing the aero-acoustical design of modern LP-turbines
Multistage turbine sound generation and propagation
Development-share of MTU Aero Engines in TP400-D6, propulsion-system
Missile firing simulation - hot gas ingestion experiments
Design and analysis of a high stage loading five-stage
Conventional and advanced coatings for turbine airfoils
On the impact of blade count reduction in a three-stage LP turbine
Unsteady aerodynamical blade row interaction in a new multistage research turbine, Part 2
Unsteady aerodynamical blade row interaction in a new multistage research turbine, Part 1
Improving 3D flow characteristics in a multistage LP-turbine, Part 2
Containment and penetration simulation in case of blade loss in a low pressure
Comparison of models to predict low engine order excitation in a high pressure turbine stage
Mistuning and coupling effects in turbomachinery bladings
Interaction of shroud leakage flow and main flow in a three-stage LP-turbine
A new method for online monitoring and trimming of pyrometer measurements
Cooling air temperature reduction in a direct transfer preswirl system
Driving the technological edge in airbreathing propulsion
Advanced high temperature turbine seals materials and designs
Experimental investigations into the nonuniform flow in a 4-stage turbine
Aerodesign and testing of an aero-mechanically highly loaded LP-turbine
Description of Thermal Effects in Aero Engines by Matrices.pdf
Generalization of the MTU 3-D Crack Propagation Criterion for anisotropic materials