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To this end, the problem on ignition of spherical granule by the stream of hot booster combustion products and the system of such granules, which simulate the filtration ignition and combustion conditions in the airbag combustion chamber, will be considered. D. Rychkov, N. Shokina, T. M. Resch, and U. Küster RAS, Novosibirsk, Russia) and the High Performance Computing Center Stuttgart (HLRS, Stuttgart, Germany) are presented. de). The technology of parallelization of the upwind LU difference scheme is considered.

De). A three-dimensional non-stationary flow in the airbag combustion chamber is numerically simulated. The technology of parallelization of the upwind LU difference scheme is considered. The future perspectives and challenges of the project are outlined. 1 Introduction The constantly increasing number of automobiles leads to the increase of traffic volume and speed regime on roads, making the problem of safety of drivers and passengers the most important one. Nowadays the airbag becomes the most reliable means in the arsenal of safety systems.

The described parallelization technology can be applied to other problems. 6 Perspectives and challenges The present paper describes the physical model and the numerical modelling of an airbag combustion chamber. It points out which steps have to be taken to the modelling of a full airbag deployment. As the calculation of a combustion process with the current model is already calculation time intensive, high performance computing systems are considered as target platforms. Within the next stages of the project the following topics will be covered: • the verification and further improvement of the physical model also using experimental data; • the extension of the simulation to the deployment process of an airbag shell including fluid-structure coupling and interaction of reaction products and the shell; • the analysis of the parallel code and its optimization for its usage on large PC clusters and vector systems.

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