Abstract
The mechanisms of primary break-up of a jet produced by a Pressure Swirl Atomizer for aircraft use is investigated. A grid study has been done together with the inlet boundary adopted to setup the simulation. The simulations are undertaken using the in-house multiphase code FS3D based on the volume of Fluid (VOF) method. All simulations were carried out on the Cray XC40 at the High Performance Computing Center Stuttgart (HLRS).
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Acknowledgements
The authors greatly appreciate the High Performance Computing Center Stuttgart (HLRS) for its support and supply of computational time on the Cray XE6 and Cray XC40 platforms under the Grant No. FS3D/11142. The authors also greatly acknowledge financial support of this project from DFG for the priority program SPP 1423 “Prozess Spray”.
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Galbiati, C., Ertl, M., Tonini, S., Cossali, G.E., Weigand, B. (2016). DNS Investigation of the Primary Breakup in a Conical Swirled Jet. In: Nagel, W., Kröner, D., Resch, M. (eds) High Performance Computing in Science and Engineering ’15. Springer, Cham. https://doi.org/10.1007/978-3-319-24633-8_22
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DOI: https://doi.org/10.1007/978-3-319-24633-8_22
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