- Identification of the aeroacoustic response of ducted low Mach number flows. n3l - Non-Normal and Nonlinear Effects in Aero- and Thermoacoustics, 2010 mehr…
- Determination of Acoustic Scattering Coefficients via Large Eddy Simulation and System Identification. In: High Performance Computing in Science and Engineering. Springer, 2010, 243-254 mehr…
- Identification of Flame Transfer Functions Using LES of Turbulent Reacting Flows. In: High Performance Computing in Science and Engineering. Springer, 2010, 255-266 mehr…
- Identification of Flame Transfer Functions from LES of a Premixed Swirl Burner. Proceedings of ASME Turbo Expo 2010: Power for Land, Sea, and Air, GT 2010, 2010 mehr…
- Determination of the stability map of a premix burner based on flame transfer functions computed with transient CFD. 4th European Combustion Meeting, 2009 mehr…
- Identification of the aeroacoustic response of a low Mach number flow through a T-joint. JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA 126 (2), 2009, 582-586 mehr…
- Determination of Acoustic Scattering Coefficients via LES and System Identification. Euromech Colloquium 540 'Large-Eddy Simulation for Aerodynamics and Aeroacoustics', 20094th Joint HLRB and KONWIHR Review and Results Workshop mehr…
- Identification of Flame Transfer Functions Using LES of Turbulent Reacting Flows. High Performance Computing in Science and Engineering, Garching 2009, Springer, 20094th Joint HLRB and KONWIHR Review and Results Workshop mehr…
- Low-order modeling of a side-branch system at low Mach numbers. 15th American Institute of Aeronautics and Astronautics/CEAS Aeroacoustics Conference (30th American Institute of Aeronautics and Astronautics Aeroacoustics Conference), 2009 mehr…
- Determination of acoustic transfer behavior via Large-Eddy-Simulation and System Identification. Linux Cluster Workshop 2008, 2008 mehr…
- CFD-Based Mapping of the Thermo-Acoustic Stability of a Laminar Premix Burner. Proceedings of the 2008 Summer Program, 2008 mehr…
- Reconstruction of Acoustic Transfer Matrices from Large-Eddy-Simulations of Complex Turbulent Flows. 14th American Institute of Aeronautics and Astronautics/CEAS Aeroacoustics Conference (29th American Institute of Aeronautics and Astronautics Aeroacoustics Conference), 2008 mehr…
- A Time-Domain Impedance Boundary Condition for Compressible Turbulent Flow. 14th American Institute of Aeronautics and Astronautics/CEAS Aeroacoustics Conference (29th American Institute of Aeronautics and Astronautics Aeroacoustics Conference), 2008 mehr…
- A Non Reflecting Boundary Condition using Wave Masking and Characteristics Based Filtering. 2nd GACM Colloquim on Computational Mechanics, 2007 mehr…
Dr.-Ing. Roland Kaess
Abgeschlossene Forschungsprojekte
The OLG-LES Approach for the Determination of Thermoacoustic Stability