The application relates to the technical field of aircrafts, and discloses an ablative particle two-phase wall turbulent flow numerical
simulation parallel computing method, equipment and medium, the method comprising the following steps: in each sub-
time step, calling a fluid
solver to calculate flow field information; using a
dynamic array to read particle information from a dynamic
linked list array one by one; calling a single particle
solver to update the particle information read by the
dynamic array, and updating the updated particle information to the dynamic
linked list array one by one; after traversing all the particles in the dynamic
linked list array, entering the next sub-
time step, until the time loop is completed, and outputting all the information of the flow field and the particles. In this way, the direct numerical
simulation of compressible ablative particle two-phase flow can be accurately realized, the problem that the prior art does not have the direct numerical
simulation of compressible particle two-phase flow at all is solved, and the blank of the direct numerical simulation of compressible ablative particle two-phase flow in China is filled.