Federica Tonti

Modelling Flame Response of a Co-axial LOx/GH2 InjectionElement to High Frequency Acoustic Forcing

M. Oschwald, J. Hardi, B. Dally, 2017 .

DLR Project TAUROS: TAU for Rocket Thrust Chamber Simulation

M. Oschwald, R. Stark, D. Schneider, 2019 .

Obtaining pseudo-OH* radiation images from CFD solutions of transcritical flames

Jaka Perovs̆ek, M. Oschwald, J. Hardi, 2021 .

Combustion dynamics in cryogenic rocket engines: Research programme at DLR Lampoldshausen

Bassam B. Dally, Scott Beinke, Michael Oschwald, 2018, Acta Astronautica.

Influence of numerical model setup on the response ofacoustically forced LOx/H2 flames

M. Oschwald, J. Hardi, S. Fechter, 2019 .

Low-order Modeling of Combustion Instability Applied to Cryogenic Propellants

M. Oschwald, J. Hardi, B. Favini, 2019 .