- Modification of Eigenmodes in a Cold-Flow Rocket Combustion Chamber by Acoustic Resonators. Journal of Propulsion and Power 35 (4), 2019, 765-779 mehr… BibTeX
- Modification of Eigenmodes in a Rocket Combustion Chamber by Acoustic Resonators under Non-Reacting Conditions. AIAA Propulsion and Energy Forum, American Institute of Aeronautics and Astronautics, 2018 mehr… BibTeX
- Influence of Acoustic Absorbers on Eigenfrequencies and Mode Shapes in a Rocket Combustor – Sonderforschungsbereich/Transregio 40 - Annual Report. , Hrsg.: Chair of Thermodynamics, Technical University of Munich, 2017, mehr… BibTeX
- Numerical Investigation of Eigenmode Damping Rates in a Single Element Rocket Combustion Chamber. 31st. International Symposium on Space Technology and Science, ISTS, 2017 mehr… BibTeX
- Thermo-Acoustic Growth Rate Determination from Numerical and Experimental Data for Rocket Engine Applications. Proceedings of the SFB/TRR 40 Summer Program (Sonderforschungsbereich Transregio 40), 2017, 67-79 mehr… BibTeX
- On the Effect of Acoustic Absorbers Coupled to Rocket Combustors. 7th European Conference for Aeronautics and Space Sciences, 2017 mehr… BibTeX
- Numerical Investigation of Indirect Noise Generation by Accelerated Vorticity. 21th AIAA/CEAS Aeroacoustics Conference, 2015 mehr… BibTeX
Dr.-Ing. Nancy Kings
Technische Universität München
Lehrstuhl für Thermodynamik (Prof. Sattelmayer)