A numerical simulation method for shock wave dynamics of cavitation compressible flow

A numerical simulation and wave mechanics technology, applied in CAD numerical modeling, sustainable transportation, design optimization/simulation, etc., can solve the problems of large difference in vapor-liquid compressibility, large numerical calculation, complex cavitation mechanism, etc. Accuracy and effectiveness in solving related engineering problems

Active Publication Date: 2021-07-27
BEIJING INSTITUTE OF TECHNOLOGYGY
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Problems solved by technology

[0003] Cavitation flow is a highly compressible compressible multiphase flow with phase change. In cavitation numerical simulation, it is often based on the assumption of phase equilibrium and incompressibility. It is considered that the velocity, pressure and temperature of the vapor / liquid phase are balanced, and the The liquid density is constant, and the incompressible cavitation numerical simulation method can predict the cavitation instability phenomena such as the growth of attached cavitation, the generation and propulsion of back jet flow, the fracture of cavitation and the process of cavitation shedding. The phenomenon of compressibility, such as cavitation-induced pressure pulsation, pressure pulse, cavitation collapse, cavitation shock wave dynamics, etc., which involves the cavitation transient load problem concerned in engineering practice, can be accurately captured. Experiments show that: cavitation The fracture and shedding process has a back jet mechanism and a shock wave mechanism. The shock wave mechanism will lead to more violent unsteady characteristics, and the shock wave mechanism is closely related to the cavitation compressibility
On the other hand, there is a non-uniform and unstable phase transition process in the cavitation flow field. The coupling of phase transition and compressibility makes the cavitation mechanism more complex and poses greater challenges to numerical calculations.
Cavitation flow has the characteristics of high density ratio between vapor and liquid, and the difference in vapor-liquid compressibility is large. At the same time, the sound velocity distribution of cavitation flow field has the characteristics of large span, from 1450m / s in pure water to 3- 5m / s, the cavitation area can reach more than 10 Mach numbers, and the introduction of compressible fluid poses new challenges for the capture of vapor-liquid free interface

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  • A numerical simulation method for shock wave dynamics of cavitation compressible flow
  • A numerical simulation method for shock wave dynamics of cavitation compressible flow
  • A numerical simulation method for shock wave dynamics of cavitation compressible flow

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Embodiment 1

[0101] Such as figure 1 As shown, a method for numerical simulation of cavitation compressible flow shock wave dynamics disclosed in this embodiment includes the following steps:

[0102] Step 1: Establish a 3D computational watershed based on 3D geometric modeling software;

[0103] For a given hydrofoil model, based on the 3D geometric modeling software, a 3D calculation watershed is established based on the size of the test section. The watershed inlet to the leading edge of the hydrofoil is the upstream flow area of ​​the hydrofoil, and the trailing edge of the hydrofoil to the watershed outlet is the downstream wake of the hydrofoil. area, in order to ensure uniform incoming flow, full development of wake and calculation efficiency, the upstream area is twice the chord length of the hydrofoil, the downstream area is five times the chord length of the hydrofoil, the spanwise distance of the hydrofoil is the width of the test section, and the hydrofoil is located at The ce...

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Abstract

The invention discloses a cavitation compressible flow shock wave dynamics numerical simulation method, which belongs to the field of cavitation compressible flow shock wave dynamics numerical simulation. The present invention establishes a three-dimensional calculation water domain based on three-dimensional geometric modeling software; divides a three-dimensional calculation water domain grid based on grid division software; establishes a cavitation compressible flow computational fluid dynamics model; sets initial boundary conditions to perform numerical calculation of a flow field in a three-dimensional calculation domain; Based on the post-processing software of the flow field, the calculation results are post-processed to obtain the unsteady evolution process of the multi-phase cavitation structure. The invention contributes to the in-depth study of the cavitation physical mechanism, can be applied to the numerical simulation fields of cavitation compressible flow and shock wave dynamics, and can solve relevant engineering problems. Cavitation compressible flow, shock wave dynamics numerical simulation engineering application fields include hydraulic machinery, ship propeller, aviation turbopump inducer, underwater supercavitation weapon application.

Description

technical field [0001] The invention relates to a numerical simulation method for cavitation compressible flow shock wave dynamics research, belonging to the field of numerical simulation of cavitation compressible flow and shock wave dynamics. Background technique [0002] Cavitation occurs in the low-pressure area of ​​high-speed water flow. It is a complex multi-phase flow involving intense phase-to-phase mass, momentum and energy exchange, phase change and turbulence. The occurrence of cavitation will induce severe pressure pulsation, vibration and noise. An in-depth understanding of the cavitation mechanism is the prerequisite for effectively suppressing the occurrence of unfavorable cavitation and avoiding cavitation damage in engineering, which has important scientific significance and engineering value. Cavitation is characterized by the generation, aggregation, and collapse of vapor cavities of different scales, and has complex interactions between cavitation / cavit...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F30/28G06F30/23G06F111/10G06F113/08G06F119/14
CPCG06F30/20Y02T90/00
Inventor 王国玉王畅畅黄彪
Owner BEIJING INSTITUTE OF TECHNOLOGYGY
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