- Frequency Domain Predictions of the Acoustic Reflection Coefficient of a Combustor Exit Nozzle with Linearized Navier-Stokes Equations. 24th International Congress on Sound and Vibration (ICSV), 2017 mehr… BibTeX
- Impact of Damper Parameters on the Stability Margin of an Annular Combustor Test Rig. Proceedings of ASME Turbo Expo, 2017 mehr… BibTeX
- Linearized Euler Equations for the Determination of Scattering Matrices for Orifice and Perforated Plate Configurations in the High Mach Number Regime. Aerospace 3 (4), 2016, 1-16 mehr… BibTeX
- Experimentally Determining the Acoustic Damping Rates of a Combustor with a Swirl Stabilized Lean Premixed Flame. Proceedings of the ASME Turbo Expo, 2015 mehr… BibTeX
- Acoustic Scattering Properties of Perforated Plates and Orifices with Stratified flow-HF8 test case. Proceedings of the 3rd Workshop on Combustion Instability Modeling, 2014 mehr… BibTeX
- Influence of Fuel-Air Mixing on Flame Dynamics of Premixed Swirl Burners. Proceedings of the ASME Turbo Expo, The American Society of Mechanical Engineers, 2014 mehr… BibTeX
- Experimental Investigation of Acousticproperties of Orifices and Perforated Plates in the High Mach Number Regime. 20th International Congress on Sound and Vibration (ICSV), 2013 mehr… BibTeX
- Design for Thermo-Acoustic Stability: Modeling of Burner And Flame Dynamics. Journal of Engineering for Gas Turbines and Power (135/11), 2013, 111502-1-7 mehr… BibTeX
- Design for thermo-acoustic stability: Procedure and database. Journal of Engineering for Gas Turbines and Power (135/12), 2013, 121507 (8 pages) mehr… BibTeX
- Design for Thermo-Acoustic Stability: Procedure and Data Base. Proceedings of the ASME Turbo Expo, 2013 mehr… BibTeX
- Design for Thermo-Acoustic Stability: Modeling of Burner and Flame Dynamics. Proceedings of the ASME Turbo Expo, 2013 mehr… BibTeX
- Comparison of the Accuracy of Time-Domain Measurement Methods for Combustor Damping. Proceedings of the ASME Turbo Expo, 2013 mehr… BibTeX
- Experimental Investigation of the Acoustic Reflection Coefficient of a Modeled Gas Turbine Impingement Cooling Section. Proceedings of the ASME Turbo Expo, 2012 mehr… BibTeX
Dipl.-Ing. Michael Wagner
Technische Universität München
Lehrstuhl für Thermodynamik (Prof. Sattelmayer)