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Flugtriebwerk
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Wet peener for aero engine blades
Using Working Parameters to Control Formation and Shape of Lotus-Type Pores
Untersuchung des Wärmeübergangs durch Einspritzkühlung für ein Höchstleistungsgetriebe
Untersuchung der Ablösung in einer Durchflussgondel bei wirbelbehafteter Zuströmung
Uncertainty Quantification for Fat-Tailed Probability Distributions in Aircraft Engine Simulations
Two-Way Blade Modeling Method for Structural Redesign of Compressor Blades
Turbulent mixing enhancement with a 10° chute mixer
Turbofan multiobjective-multipoint optimization for UAV/UCAV applications
Titanium Aluminide Turbine Toolbox : Teilprojekt Access : Schlussbericht zum Verbundprojekt TATT
Time-Varying Operating Condition–Based Prediction of the Remaining Useful Life for Aeroengine
TI makes $58 million aerospace acquisition
Thermal Performance of Transonic Cooled Tips in a Turbine Cascade
Technology secures competitive edge in jet engine race
System Identification for Propellers at High Incidence Angles
Supply-chain solution agreement
Stufenentwurf mit stabilisierenden Gehäuseeinbauten : 1.1.6a : Schlussbericht Teil I und II
Stress concentration in compressor blades at their damage by foreign objects
Statistical estimation of multiple faults in aircraft gas turbine engines
Stabilisation of Hydrodynamic Instabilities by Critical Layers in Acoustic Lining Boundary Layers
Special blast cabinet prepares aero engine components
Sound Production due to Swirl–Nozzle Interaction: Model-Based Analysis of Experiments