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Euler-Lagrange Simulation of a LOX/H2 Model Combustor with Single Shear Coaxial Injector

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High Performance Computing in Science and Engineering '10

Abstract

In this paper a mixed Euler-Lagrange approach is used for a 3D simulation of a LOX/H2 model rocket combustor with a single shear coaxial injector. The specific test case presented is the MASCOTTE combustor at 10 bar pressure in the so called A-10 configuration. The simulation of the gas phase is conducted with the scientific code TASCOM3D which works in an Eulerian mode while the liquid fuel droplets are treated by the scientific code SPRAYSIM in a Lagrangian framework. The two codes and the coupling mechanisms are explained and results of a preliminary simulation will be presented. At the end an outlook is given focusing on how to obtain an even more accurate representation of the experiment in subsequent simulations. Finally some comments on the computational costs of the calculations and the performance of the two codes on the NEC SX-9 are given.

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Authors and Affiliations

  1. Institut für Verbrennungstechnik der Luft- und Raumfahrt, Universität Stuttgart, Pfaffenwaldring 38-40, 70569, Stuttgart, Germany

    Markus Lempke, Peter Gerlinger & Manfred Aigner

  2. Institut für Verbrennungstechnik, DLR Köln, Linder Höhe, 51147, Köln, Germany

    Michael Rachner

Authors
  1. Markus Lempke
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  2. Peter Gerlinger
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  3. Michael Rachner
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  4. Manfred Aigner
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Corresponding author

Correspondence to Markus Lempke .

Editor information

Editors and Affiliations

  1. Zentrum für Informationsdienste und, Hochleistungsrechnen (ZIH), TU Dresden, Dresden, 01062, Germany

    Wolfgang E. Nagel

  2. , Abt. Angewandte Mathematik, Universität Freiburg, Hermann-Herder-Str. 10, Freiburg, 79104, Germany

    Dietmar B. Kröner

  3. Stuttgart (HLRS), Universität Stuttgart, Höchstleistungsrechenzentrum, Nobelstraße 19, Stuttgart, 70569, Germany

    Michael M. Resch

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Lempke, M., Gerlinger, P., Rachner, M., Aigner, M. (2011). Euler-Lagrange Simulation of a LOX/H2 Model Combustor with Single Shear Coaxial Injector. In: Nagel, W., Kröner, D., Resch, M. (eds) High Performance Computing in Science and Engineering '10. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-15748-6_16

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