Two Compressibility Corrections to Flamelet/Progress Variable Model for Supersonic Combustion

Shan, Fanli; Hou, Lingyun; Chen, Zheng; Su, Bingwei

doi:10.2514/6.2017-2163

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“…The multi-scale combustion in leadingedge engines (named MuSCLE) is a large-scale CFD parallel software developed by Beijing Institute of Spacecraft Systems Engineering. The software is oriented to structured multi-block, dynamic adaptive, and unstructured grids [22][23][24] . MuSCLE can be used to guide engineering designs and study key scientific issues in major research projects through high-precision multiscale algorithms.…”

Section: Applicationmentioning

confidence: 99%

Brief introduction of TianHe exascale prototype system

Wang

Lü

Chen

et al. 2021

Tinshhua Sci. Technol.

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Facing the challenges of the next generation exascale computing, National University of Defense Technology has developed a prototype system to explore opportunities, solutions, and limits toward the next generation Tianhe system. This paper briefly introduces the prototype system, which is deployed at the National Supercomputer Center in Tianjin and has a theoretical peak performance of 3.15 Pflops. A total of 512 compute nodes are found where each node has three proprietary CPUs called Matrix-2000+. The system memory is 98.3 TB, and the storage is 1.4 PB in total.

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Section: Applicationmentioning

confidence: 99%