2019
DOI: 10.1016/j.compfluid.2019.104310
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Analysis of transient combustion with the use of contemporary CFD techniques

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Cited by 25 publications
(10 citation statements)
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“…The governing Equations ( 1)-( 7) were integrated via the second-order predictor/corrector method described in [32]. To perform mathematical modeling of low-Mach gasdynamics we implemented algorithms described in [32] in the in-house code, which was thoroughly tested and validated previously on a vast variety of gas dynamics and combustion problems [11,33]. The computational mesh cell size was equal to ∆x = 0.2 mm, the overall amount of cells was 45,000.…”
Section: Methodsmentioning
confidence: 99%
“…The governing Equations ( 1)-( 7) were integrated via the second-order predictor/corrector method described in [32]. To perform mathematical modeling of low-Mach gasdynamics we implemented algorithms described in [32] in the in-house code, which was thoroughly tested and validated previously on a vast variety of gas dynamics and combustion problems [11,33]. The computational mesh cell size was equal to ∆x = 0.2 mm, the overall amount of cells was 45,000.…”
Section: Methodsmentioning
confidence: 99%
“…The characteristic decomposition method underlying the CABARET technique allows for a straightforward description of the inflow and outflow boundary conditions via the relationships between characteristics. Recently, this numerical technique was adopted by several authors for the numerical analysis of combustible systems, and they showed its usefulness in solving the problems of reactive gas dynamics [ 25 , 26 , 27 ]. In particular, the chosen numerical technique is thoroughly validated for hydrogen–air flames in [ 25 ].…”
Section: Problem Setupmentioning
confidence: 99%
“…Recently, this numerical technique was adopted by several authors for the numerical analysis of combustible systems, and they showed its usefulness in solving the problems of reactive gas dynamics [ 25 , 26 , 27 ]. In particular, the chosen numerical technique is thoroughly validated for hydrogen–air flames in [ 25 ]. Moreover, it reproduces the non-steady effects in flame development well and predicts with high accuracy such a phenomenon as the deflagration-to-detonation transition [ 27 ] (the calculations agree well with the available experimental data).…”
Section: Problem Setupmentioning
confidence: 99%
“…The combustion reaction is an important branch of chemical reaction, and combustion reactions are composed of complex thermal and chemical processes, which are often coupled to varying degrees. Although the continuous fluid hypothesis has always been the basis of most theoretical and numerical studies in the field of combustion, the physical principles of combustion still rely on molecular processes, such as diffusion and chemical reactions. Especially for the combustion process of ramjet engines, more microscale molecular dynamics information is needed to describe the shock waves, thermal nonequilibrium, and chemical reactions caused by high-speed incoming gases. …”
Section: Introductionmentioning
confidence: 99%
“…Among hydrocarbon fuels, hydrogen and methane are generally the most commonly used fuels. As a commonly used fuel, there have been many studies and applications of the combustion mechanism and computational fluid dynamics (CFD) simulation of hydrogen. ,,, Indeed, the elementary reaction of H 2 combustion is the core part of the description of the combustion mechanism of all hydrocarbons and oxygenated hydrocarbon fuels. In addition to using reaction kinetic mechanisms based on rate constants of the elementary reaction to consider chemical reactions in hydrogen combustion, DSMC, DMS, and reactive force field-based molecular dynamics (MD) methods have also been used in the process of hydrogen combustion.…”
Section: Introductionmentioning
confidence: 99%