Method for acquiring non-local variable information of boundary layer of unstructured grid
An unstructured grid, variable information technology, applied in the field of boundary layer transition prediction in fluid mechanics, can solve problems such as limiting transition mode, application of transition criterion method, and difficulty in improving prediction accuracy.
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Embodiment 1
[0080] This example describes a specific embodiment of the application of the method of the present invention to the T3A plate.
[0081] figure 1 It is a flowchart of the method of the present invention. figure 2 It is a schematic diagram of grid preprocessing by the method of the present invention. image 3 It is a schematic diagram of modifying the outer edge of the boundary layer based on the unstructured grid in the present invention. Based on this, the specific implementation of the present invention in a specific application scenario is described.
[0082] The calculation domain of the T3A plate is a rectangle with length L=1000mm, height H=150mm, and the distance between the entrance and the front edge of the plate is 80mm. The calculation adopts mixed grids, the structured grids inside the boundary layer, the unstructured grids outside the boundary layer, and the grids near the wall and the front edge of the plate are densified. In the boundary layer, there are 11...
Embodiment 2
[0086] This example describes the specific implementation of applying the method of the present invention to the calculation model of the swept cylinder.
[0087] The cylinder radius is 30mm and the sweep angle is 50°. The free flow and wall conditions are: Ma ∞ = 3, Re ∞ =2.83×10 7 / m,T ∞ =121.42K,T w = 300K. The grid height of the first layer of the wall guarantees y + =1, the grid near the shock wave position is denser. The wall is set as a non-slip solid wall edge strip, with periodic edge strips on both sides.
[0088] According to the method for grid preprocessing and obtaining boundary layer information provided by the present invention, the cross flow velocity distribution in the boundary layer of the swept cylinder is obtained. Figure 6 is the azimuth Dimensionless cross-flow velocity w / u obtained in the range e Compared with the literature results of Balakumar et al., it can be seen that the difference The cross-flow velocity profile of the station is bas...
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