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In order to describe partially premixed supersonic combustion numerically, G/Z flamelet model is developed and compared with finite rate model in hybrid RANS/LES simulation to study the strut-injection supersonic combustion flow field designed by the German Aerospace Center.
Booked for simulation to boot.
We used a gravity simulation to have them bounce.
Try running a simulation to prepare them.
This paper motivates the use of Ptolemy II software environment for mode ling and simulation of heterogeneous control systems.
The goal of this simulation was to measure LE's fairness with SACK.
Fondation Le Roch les Mousquetaires to Pascale Cossart.
Association Française Contre les Myopathies to Gideon Dreyfuss.
Of course, to achieve such a result full integration between mode ling and simulation should be achieved.
Le moved on to financials.
LE contributed to study design.
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