TY - GEN
T1 - Direct numerical simulation of shock-induced drop breakup with a sharp-interface-method
AU - Kaiser, Jakob W.J.
AU - Adami, Stefan
AU - Adams, Nikolaus A.
N1 - Funding Information:
The lead author is supported by the German Research Foundation (Deutsche Forschungsgesellschaft, DFG). The second and third authors acknowledge funding by the European Research Council (ERC) under the European Union’s Horizon 2020 research and innovation program (grand agreement No. 667483) The authors gratefully acknowledge the Gauss Centre for Supercomputing e.V. (www.gauss-centre.eu) for funding this project by providing com-
PY - 2017
Y1 - 2017
N2 - We present two-and three-dimensional numerical results of the shock-induced breakup of a liquid droplet in air. We apply a conservative interface interaction model for sharp-interface representation and a block-based multi-resolution scheme to adaptively refine our mesh. Numerical modeling effects, such as the flux reconstruction scheme and the use of a scale separation model, that treats non-resolved interface segments, are investigated. Similarly as a previous study (Meng, 2016), we identify two dominant mechanisms of droplet breakup at certain Mach numbers-flattening of the droplet and sheet stripping-occurring simultaneously and influencing each other in our simulations. Three-dimensional simulations show the flattening mechanism and the mushroom-like deformation of the droplet. They also explain the occurrence of a recirculation zone in the droplet wake. The two-dimensional simulations already exhibit the sheet stripping mechanism, which occurs during and after droplet flattening. Small sheets emerge from both the upstream and the downstream side of the 2D droplet, while the main sheet develops at the droplet equator.
AB - We present two-and three-dimensional numerical results of the shock-induced breakup of a liquid droplet in air. We apply a conservative interface interaction model for sharp-interface representation and a block-based multi-resolution scheme to adaptively refine our mesh. Numerical modeling effects, such as the flux reconstruction scheme and the use of a scale separation model, that treats non-resolved interface segments, are investigated. Similarly as a previous study (Meng, 2016), we identify two dominant mechanisms of droplet breakup at certain Mach numbers-flattening of the droplet and sheet stripping-occurring simultaneously and influencing each other in our simulations. Three-dimensional simulations show the flattening mechanism and the mushroom-like deformation of the droplet. They also explain the occurrence of a recirculation zone in the droplet wake. The two-dimensional simulations already exhibit the sheet stripping mechanism, which occurs during and after droplet flattening. Small sheets emerge from both the upstream and the downstream side of the 2D droplet, while the main sheet develops at the droplet equator.
UR - http://www.scopus.com/inward/record.url?scp=85033225527&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:85033225527
T3 - 10th International Symposium on Turbulence and Shear Flow Phenomena, TSFP 2017
BT - 10th International Symposium on Turbulence and Shear Flow Phenomena, TSFP 2017
PB - International Symposium on Turbulence and Shear Flow Phenomena, TSFP10
T2 - 10th International Symposium on Turbulence and Shear Flow Phenomena, TSFP 2017
Y2 - 6 July 2017 through 9 July 2017
ER -