Large-eddy simulation (LES) of combustion in aero-engine combustors
Numerical analysis of flame acoustic response and development of associated methods
Characteristics based boundary conditions for compressible flow simulations
Thermoacoustic instabilities
Duct acoustics
The figure illustrates the reacting flow field in a lean-burn aero-engine combustor within the SCARLET (SCaled Acoustic Rig for Low Emission Technology) rig by Rolls-Royce Deutschland. This setup offers exclusive data on the acoustic response of full-scale aero-engine injectors under realistic conditions. The image, generated from reacting compressible large-eddy simulation data, offers crucial insights into intricate interactions influencing the observed flame response. It serves as a foundation for developing advanced post-processing strategies and innovative simulation approaches.
The figure illustrates the reacting flow field in a lean-burn aero-engine combustor within the SCARLET (SCaled Acoustic Rig for Low Emission Technology) rig by Rolls-Royce Deutschland. This setup offers exclusive data on the acoustic response of full-scale aero-engine injectors under realistic conditions. The image, generated from reacting compressible large-eddy simulation data, offers crucial insights into intricate interactions influencing the observed flame response. It serves as a foundation for developing advanced post-processing strategies and innovative simulation approaches.
Reacting and non-reacting LES and RANS simulations using Rolls-Royce Germany combustion-oriented CFD software PRECISE-UNS
Acoustic post-processing of numerical and experimental datasets using in-house tools
Acoustic network modeling using in-house tools
All publications are listed in the publication list:
The integrated database, TUbiblio of TU Darmstadt, is currently being revised, which is why the author's complete publication list can currently only be accessed though the links above.
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