Towards a design tool for reacting multi-phase flows in porous structures
9th Int. Conference on Development Trends in space Propulsion Systems
2015
Injector Characterization for a GOX-GCH4 Single Element Combustion Chamber
EUCASS Advances in Aerospace Sciences, Progress in Propulsion Physics Vol. 8
Torus Press
2015
Computing supersonic non-pre-mixed turbulent combustion by an SMLD flamelet progress variable
Journal of Hydrogen Energy
2015
The effect of injector geometry on the flashing spray with cryogenic propellants
6th European Conference for Aeronautics and Space Sciences (EUCASS)
2015
Analysis of Reenrty Vehicle Flight Physics
6th European Conference for Aeronautics and Space Sciences (EUCASS)
2015
Numerical Investigation of 3D Effects in Hartmann-Sprenger Tubes
6th European Conference for Aeronautics and Space Sciences (EUCASS)
2015
Collaborative Research Center TRR 40 - Technological Foundations for the Design of Thermally and Mechanically highly loaded Components of future Space Transportation Systems
6th European Conference for Aeronautics and Space Sciences (EUCASS)
2015
Heat Flux Evaluation Methods for a Single Element Heat Sink Chamber
6th European Conference for Aeronautics and Space Sciences (EUCASS)
2015
Comparison of Single Element Rocket Combustion Chambers with Round an Square Cross Sections
6th European Conference for Aeronautics and Space Sciences (EUCASS)
2015