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Numerical simulations of gaseous detonation propagation using different supercomputing architechtures. (English) Zbl 1404.80010

Summary: The aim of the present study is to calculate the process of detonation combustion of gas mixtures in engines. Development and verification of 3D transient mathematical model of chemically reacting gas mixture flows incorporating hydrogen is performed. Development of a computational model based on the mathematical one for parallel computing on supercomputers incorporating CPU and GPU units is carried out. Investigation of the influence of computational grid size on simulation precision and computational speed is performed. Investigation of calculation runtime acceleration is carried out subject to variable number of parallel threads on different architectures and implying different strategies of parallel computation.

MSC:

80A25 Combustion
65Y10 Numerical algorithms for specific classes of architectures
76M25 Other numerical methods (fluid mechanics) (MSC2010)
76L05 Shock waves and blast waves in fluid mechanics
80M25 Other numerical methods (thermodynamics) (MSC2010)

Software:

CUDA; CHEMKIN; AUSM; LOGOS
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Full Text: DOI

References:

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