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IN2HDV
Full article
AG Turbo 2020 4.1.5
Optimization of Linear Simulation Techniques for the Aeroelastic Design of Coupled Turbine Blades
Full article
TurboVaLd (Validation of turbulence models using Laser diagnostics)
Within the DLR internal project TurboVaLd, complex flows with relevant effects for turbomachinery are investigated in depth using optical Laser diagnostics.
Full article
SAMURAI (Synergy of Advanced Measurement Techniques for Unsteady and High Reynolds Number Aerodynamic Investigations)
Within SAMURAI, amongst others, a large field dataset of the ground-based engine jet of the DLR research aircraft ATRA will be made available with various image-based experimental measurement systems. These are used to extent the aerodynamic, -elastic and -acoustic knowledge of these two complex flow systems and for the validation of accompanying advanced numerical simulations.
Full article
MTU-sponsorship: Non-Reflecting boundary conditions for the turbomachinery flow solver TRACE
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COOREFLEX-turbo Cooling Project 3.4.3
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R&E TURB
In the framework of the joint project R&E TURB (Robust and efficient turbines for turbofans, geared turbofans and next generation turboshaft engines) of the Aeronautics Research Program IV the Numerical Methods department is involved in the work package 3 (Next Step Calculation-/Optimization methods) with the development of the simulation system TRACE.
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HEAT
The DLR internal Project HEAT investigates the thermal budget of turbine blades.
Full article
OmniTurb
The aim of the DLR-project OmniTurb is to be able to do “Design, optimization and measurement of a two stage high pressure turbine with combustion chamber simulator”.
Full article
LeiLa
The main subject of this project is to reduce the noise generated by the fan, the combustion chamber and the turbine in all phases of a flight (take-off, overflight, and landing).
Full article
PERFEKT
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GASPI
The department Numerical Methods is involved in BMBF-funded project GASPI in the field of high-performance computing. The aim of the project is to develop a high-performance library for unilateral and asynchronous communication on the basis of the Fraunhofer PGAS API.
Full article
Digital-X
The target course of the program system Digital-X is the computer-based design of aircraft and the virtual flight testing of these systems. The long-term goal is the development of an integrated software platform for multidisciplinary analysis and optimization.
Full article
COOREFLEX-Turbo-4.2.4 Flutter Analysis for Embedded Blade Rows
This project focuses on the development and application of a frequency domain method for the analysis of the aerodynamic excitation of blade vibration taking into account the effect of adjacent blade rows.
Full article
IL-Turb
Full article
MTU-sponsorship
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