Article ID Journal Published Year Pages File Type
1714347 Acta Astronautica 2015 18 Pages PDF
Abstract

The aim of the present study is to investigate problems of numerical simulations precision and stochastic errors accumulation in solving problems of detonation or deflagration combustion of gas mixtures in rocket engines. Computational models for parallel computing on supercomputers incorporating CPU and GPU units were tested and verified. Investigation of the influence of computational grid size on simulation precision and computational speed was performed. Investigation of accumulation of errors for simulations implying different strategies of computation were performed.

Related Topics
Physical Sciences and Engineering Engineering Aerospace Engineering
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