A New Velocity Correction Method for Projection Immersion Boundary Method
A correction method and boundary technology, applied in the direction of instruments, computing, electrical digital data processing, etc., can solve problems such as low computing efficiency, heavy computing workload, and abnormally complex computing, so as to improve computing efficiency, save computing resources, and ensure energy conservation effect
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Embodiment 1
[0056] Embodiment 1: as Figure 1-5 As shown, a new speed correction method of projected immersion boundary method, the specific steps of the method are as follows:
[0057] A. Invoke the mesh division module, using two sets of grids: flow field area and solid boundary area; the flow field area is discretized with Cartesian grid under the Euler description, and the solid boundary area is discretized under the Lagrangian description. The volume curve grid is discretized, and the flow field area includes the pure flow field area and the secondary flow field area;
[0058] B. Call the flow field velocity prediction module, and use the step-by-step projection method to solve the flow control equation of the incompressible viscous Newtonian fluid, and obtain the predicted value of the original variable in the flow field area;
[0059] C. Call the Euler grid point attribute judgment module to judge whether the Euler grid point belongs to the solid internal area or the solid externa...
Embodiment 2
[0100] Embodiment 2: as Figure 1-5 As shown, a new speed correction method of projected immersion boundary method, the specific steps of the method are as follows:
[0101] The flow field area includes a turbine movable guide vane airfoil, the length of its chord line is L, the maximum thickness is D, the calculation area is 15L×10L, and the coordinate origin is located at the midpoint of the chord line. The flow Reynolds number is defined as Re=ρU b D / μ=200, the time step Δt=0.002, and the discretization interval of the square column boundary is 0.01L.
[0102] S1: Meshing
[0103] The flow field area (including the fluid and turbine movable guide vane airfoil area) is divided into Cartesian grids under the Euler description. The grids are uniform quadrilateral grids, and the grid spacing is h=0.01L. And the flow field area is divided into a pure flow field area and a secondary flow field area. In this example, the secondary flow field area is 1.4L×1.4L, and the center of...
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