This invention relates to the field of
simulation and computation technology, specifically to a
simulation analysis method and apparatus for aircraft in-flight water drop based on VOF-DPM. It addresses the problems of actual flight tests being significantly affected by weather, incurring high manpower and material costs, and difficulties in measuring local dynamic physical quantities, as well as the time-consuming nature and scale-effect errors in scaled-down model tests. The method includes setting up a flow field domain, dividing it into an air domain and a water domain; spatially discretizing the flow field domain based on a Cartesian
octree grid; effectively capturing the
free interface of the gas-liquid two-phase flow using a VOF-DPM combined h-type refined adaptive grid; and progressively refining the local grid of the Cartesian
octree grid, with a grid refinement standard of 2 in each direction. x The physical parameters of the flow field are initialized; the position and shape of the phase interface are captured using the VOF method based on grid resolution; and the free-moving droplets are simulated to realize the
simulation analysis of airborne water droplets from aircraft.