11-04-2023 дата публикации
Номер: CN115952605A
Принадлежит:
The invention relates to the technical field of aircrafts, and discloses a numerical simulation method and device for the aperiodic dynamic process of ablated particles and a medium, and the method comprises the steps: reading particle information from a dynamic linked list array; deleting particle information leaving the boundary of the numerical simulation calculation domain; and dynamically allocating the memory to the dynamic linked list array of the wall surface, so that the particles are re-released from the wall surface. Therefore, the method can be coupled with a two-phase wall turbulence mode of any compressible particle, when the particle leaves the boundary of the numerical simulation calculation domain, the dynamic linked list array is adopted to delete the leaving particle memory, and the particle memory is redistributed, so that the particle can be continuously released from the wall surface; therefore, the aperiodic boundary conditions of the ablative particles in the boundary ...
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