1/7/13    15:30 - 18:50
PP.29: Combustion Modeling
MoA04
Room: Holiday Inn - Forum 6
Chair: Christian Stemmer
CoChair: Mohan Varma
Rapporteur: to be confirmed
The Role of Presumed Probability Density Function in the Simulation of Non-premixed Turbulent Combustion
A. Coclite, G. Pascazio, P. De Palma and L. Cutrone


Multiscale Aviation Kerosene Modeling: from ab initio Quantum Chemistry to the Combustion Chamber Simulations
V.L. Kovalev, S.O. Adamson, A.S. Vetchinkin and A.V. Vagner


Investigation of different modeling approaches for CFD simulation of high pressure rocket combustors
B. Ivancic, H. Riedmann, M.  Frey, O.  Knab, S. Karl and K. Hannemann


Numerical Investigation of Spray Combustion and Flow in LOX/H2 Subscale Rocket Combustors
H. Riedmann, B. Kniesner, M. Frey and C-D. Munz


A Posteriori Computation of OH* Radiation from Numerical Simulations in Rocket Combustion Chambers
T. Fiala and T. Sattelmayer


Large Eddy Simulation of supersonic non-reactive and reactive flows with an immersed boundary method (*)
L. Bouheraoua, G. Ribert, P. Domingo and G. Lartigue


Development and Evaluation of Transient Analysis Tool for Rocket Engine
A. Ogawara and C. Sezaki


Numerical simulations of slame of single co-axial injector
V.P. Zhukov and M. Feil