- Validation of the computation of rocket nozzle admittances with linearized euler equations. EUCASS Proceedings Series - Advances in AeroSpace Sciences 4, 2013, 135-148 more… BibTeX
- A Conceptional Approach for the Prediction of Thermoacoustic Stability in Rocket Engines. 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, San Jose, California, USA, 2013 more… BibTeX
- Dämpfung akustischer Wellen durch Absorber in Raketentriebwerken. 61. Deutscher Luft- und Raumfahrtkongress, 2012 more… BibTeX
- Sonderforschungsbereich/Transregio 40: Brennkammer. 60. Deutscher Luft- und Raumfahrtkongress, 2011 more… BibTeX
- Influence of Scaling Rules on Loss of Acoustic Energy. Journal of Spacecraft and Rockets 48 (3), 2011, 498-506 more… BibTeX
- Numerical Determination of Nozzle Admittances in Rocket Engines. In: New Results in Numerical and Experimental Fluid Mechanics VII. Springer-Verlag Berlin Heidelberg, 2010, 579-586 more… BibTeX
- Rapid approach for the prediction of complex acoustic resonance frequencies in rocket combustion chambers. 2nd REST Modeling Workshop, 2010 more… BibTeX
- Vorticity Feed Back Model. 2nd REST Modeling Workshop, Ottobrunn, Germany, 2010 more… BibTeX
Dr.-Ing. Daniel Morgenweck
Technical University of Munich
Chair of Thermodynamics (Prof. Sattelmayer)