Numerical simulation of the flow over a hypersonic waverider using the method for splitting into physical processesстатья
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Дата последнего поиска статьи во внешних источниках: 17 января 2018 г.
Аннотация:The aim of the study is to obtain hypersonic waverider aerodynamic characteristics over the angle-of-attack range from 0 to 10 at Mach 4. The simplified virtual model of the waverider was designed. The Navier-Stokes equations solution was performed using computer code into which the method for splitting into physical processes was implemented. The unstructured grid was used in the computational process.