A Method for Identifying Turbulent Flow Regions
A region identification and turbulence technology, applied in the field of computational fluid dynamics, can solve the problems of no eddy viscosity coefficient and limited application range, and achieve the effect of expanding the scope of application and simplifying the calculation process.
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[0054] On the basis of Example 1, for the supersonic flow field containing the shock wave, the shock wave detection factor φ (the shock wave detection factor comes from the open literature) is added, thereby the turbulent region identification function is corrected as:
[0055]
[0056]
[0057]
[0058]
[0059] C1=0.1, C2=3.0, C3=4.0, C4=3.0, C5=2.0, ε=10 -20
[0060] here,
[0061] is the velocity vector of the flow field,
[0062] ω is the absolute value of vorticity.
[0063] By considering the factors of the shock wave in the high-speed flow, the turbulence identification function formula (ii) proposed by the present invention enables the method to be effectively applied to the supersonic flow field.
[0064] Such as Figure 4 Shown is the application of formula (ii) of the present invention in supersonic (Mach number Ma=1.8) jet flow large eddy simulation (using dynamic Smagorinsky model). Depend on Figure 4 It can be seen that the present invention...
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