Application highlights of the DSMC Analysis Code (DAC) software for simulating rarefied flows, The DSMC Analysis Code (DAC) software represents the National Aeronautics and Space Administration’s (NASA’s) state-of-the-art implementation of the Direct Simulation Monte Carlo (DSMC) method of Bird for simulating three-dimensional flows. It is utilized by NASA, as well as other organizations from the government, commercial and academic sectors to simulate rarefied gas dynamic environments with complex geometric or flowfield characteristics. The fundamentals of the DSMC method are presented to provide the necessary groundwork for a discussion of the important features of the DAC software. The accuracy of the implementation is demonstrated through a collection of previously documented results, where simulations performed using the DAC software are compared to other codes as well as actual flight derived data. A compilation of diverse applications is used to highlight the software’s underlying flexibility and the significance of this capability to support important NASA missions.

References in zbMATH (referenced in 11 articles , 1 standard article )

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  1. Yang, L. M.; Shu, C.; Yang, W. M.; Wu, J.: An improved three-dimensional implicit discrete velocity method on unstructured meshes for all Knudsen number flows (2019)
  2. Jun, Eunji; Gorji, M. Hossein; Grabe, Martin; Hannemann, Klaus: Assessment of the cubic Fokker-Planck-DSMC hybrid method for hypersonic rarefied flows past a cylinder (2018)
  3. Cai, Chunpei; He, Xin; Zhang, Kai: Comprehensive studies on rarefied jet and jet impingement flows with gas-kinetic methods (2017)
  4. Jambunathan, Revathi; Levin, Deborah A.: Advanced parallelization strategies using hybrid MPI-CUDA octree DSMC method for modeling flow through porous media (2017)
  5. Kumar, Rakesh; Chinnappan, Arun Kumar: Development of a multi-species, parallel, 3D direct simulation Monte-Carlo solver for rarefied gas flows (2017)
  6. Hssikou, Mohamed; Baliti, Jamal; Alaoui, Mohammed: The planar Couette flow with slip and jump boundary conditions in a microchannel (2016)
  7. Lo, Ming-Chung; Su, Cheng-Chin; Wu, Jong-Shinn; Tseng, Kun-Chang: Modelling rarefied hypersonic reactive flows using the direct simulation Monte Carlo method (2015)
  8. Turansky, Craig; Argrow, Brian: Volumetric geometry for DSMC and the Voldipar code (2015)
  9. Zhang, Chonglin; Schwartzentruber, Thomas E.: Robust cut-cell algorithms for DSMC implementations employing multi-level Cartesian grids (2012)
  10. Zhang, Wen-pu; Han, Bo; Zhang, Cheng-yi: Spacecraft aerodynamics and trajectory simulation during aerobraking (2010)
  11. LeBeau, G. J.; Lumpkin, F. E. III: Application highlights of the DSMC analysis code (DAC) software for simulating rarefied flows (2001)