TY - GEN
T1 - Robust Cut-cell algorithms for DSMC implementations employing multi-level Cartesian grids
AU - Zhang, Chonglin
AU - Schwartzentruber, Thomas E.
PY - 2011
Y1 - 2011
N2 - Robust cut-cell algorithms are detailed for general multi-level Cartesian grid direct simulation Monte Carlo (DSMC) implementations. The essential components of the cut-cell algorithms, necessary to achieve the overall functionality of general multi-level Cartesian grid DSMC implementation, are discussed in detail. Different approaches for each component of the cut-cell algorithms are elaborated and compared, based on time effciency, robustness and ease of implementation. Special situations that arise in sorting the surface triangles, calculating the cut-cell volume, and identifying multiple cut-cells resulting from single regular Cartesian cell, are handled in the algorithms, and their effects on the overall simulation results are analyzed using test cases. Simulations for a Mach number 20.2 N2 gas flowing over a spherical-blunted Planetary Probe are conducted as one demonstration, and overall good agreements with experimental results are achieved for heat flux over the Planetary Probe surface. Rarefied flow over a geometry resembling the MIR Space Station is also conducted, to demonstrate the ability of the proposed cut-cell algorithms in handling complex geometries. The time required to cut the background Cartesian cells from the surface mesh and to calculate the volume of the resulting cut-cells is shown to be comparable to the time cost for one DSMC simulation time step for cases considered.
AB - Robust cut-cell algorithms are detailed for general multi-level Cartesian grid direct simulation Monte Carlo (DSMC) implementations. The essential components of the cut-cell algorithms, necessary to achieve the overall functionality of general multi-level Cartesian grid DSMC implementation, are discussed in detail. Different approaches for each component of the cut-cell algorithms are elaborated and compared, based on time effciency, robustness and ease of implementation. Special situations that arise in sorting the surface triangles, calculating the cut-cell volume, and identifying multiple cut-cells resulting from single regular Cartesian cell, are handled in the algorithms, and their effects on the overall simulation results are analyzed using test cases. Simulations for a Mach number 20.2 N2 gas flowing over a spherical-blunted Planetary Probe are conducted as one demonstration, and overall good agreements with experimental results are achieved for heat flux over the Planetary Probe surface. Rarefied flow over a geometry resembling the MIR Space Station is also conducted, to demonstrate the ability of the proposed cut-cell algorithms in handling complex geometries. The time required to cut the background Cartesian cells from the surface mesh and to calculate the volume of the resulting cut-cells is shown to be comparable to the time cost for one DSMC simulation time step for cases considered.
UR - https://www.scopus.com/pages/publications/85087598569
UR - https://www.scopus.com/pages/publications/85087598569#tab=citedBy
U2 - 10.2514/6.2011-3314
DO - 10.2514/6.2011-3314
M3 - Conference contribution
AN - SCOPUS:85087598569
SN - 9781624101465
T3 - 42nd AIAA Thermophysics Conference
BT - 42nd AIAA Thermophysics Conference
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - 42nd AIAA Thermophysics Conference 2011
Y2 - 27 June 2011 through 30 June 2011
ER -