High-fidelity chaotic polynomial correction method suitable for CFD uncertainty quantification

A chaotic polynomial, high-fidelity technology, applied in the field of computational fluid dynamics, can solve problems such as difficulty in evaluation, increased computational requirements, and limited applications, and achieve the effect of saving computational costs

Pending Publication Date: 2020-12-01
CALCULATION AERODYNAMICS INST CHINA AERODYNAMICS RES & DEV CENT
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Problems solved by technology

As the dimension of uncertainty parameters increases, the computational demands of these two methods increase sharply, which limits their application in engineerin

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  • High-fidelity chaotic polynomial correction method suitable for CFD uncertainty quantification
  • High-fidelity chaotic polynomial correction method suitable for CFD uncertainty quantification
  • High-fidelity chaotic polynomial correction method suitable for CFD uncertainty quantification

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Embodiment Construction

[0036] All features disclosed in this specification, or steps in all methods or processes disclosed, may be combined in any manner, except for mutually exclusive features and / or steps.

[0037] Any feature disclosed in this specification (including any appended claims, abstract and drawings), unless expressly stated otherwise, may be replaced by alternative features which are equivalent or serve a similar purpose. That is, unless expressly stated otherwise, each feature is one example only of a series of equivalent or similar features.

[0038] Such as figure 1 As shown, this embodiment includes the following steps:

[0039] S1: Obtain a low-fidelity model through calculation at the low-fidelity model level, and establish a rough chaotic polynomial expansion;

[0040] S2: Perform deterministic calculations at the high-fidelity model level;

[0041] S3: Correct the low-fidelity model established in S1 to obtain the final high-fidelity model.

[0042] Taking the analysis of...

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Abstract

The invention discloses a high-fidelity chaotic polynomial correction method suitable for CFD uncertainty quantification, and the method is characterized in that the method comprises the steps of obtaining a low-fidelity model at a low-fidelity model level through calculation, and building a rough chaotic polynomial expansion; performing a small amount of calculation on a high fidelity model level; and correcting the low-fidelity model to obtain a final high-fidelity correction model. According to the invention, the statistical information of the obtained high fidelity correction model is slightly different from that of the original high fidelity model; the mean value difference is smaller than three ten thousandths and can be ignored, the error requirement of engineering application is completely met, the calculation time needed by the high-fidelity model established through the method is about 40% of that of an original method, and the calculation cost is greatly saved.

Description

technical field [0001] The invention relates to the field of computational fluid dynamics, in particular to a high-fidelity chaotic polynomial correction method suitable for CFD uncertainty quantification. Background technique [0002] CFD (Computational Fluid Dynamics, Computational Fluid Dynamics) has played an increasingly important role in aerospace, water and land transportation, energy power, atmosphere and ocean and other fields. However, there are a large number of uncertain parameters in CFD, such as turbulence model coefficients, thermophysical parameters and so on. This also leads to significant uncertainties in the simulation results. Uncertain factors may lead to product performance fluctuations, or even functional failure. NASA has investigated 2,500 in-orbit vehicle failures, about 52% of which were caused by uncertain factors. Therefore, in the process of aircraft optimization design and performance evaluation, it is necessary to quantify the influence of ...

Claims

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Application Information

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IPC IPC(8): G06F30/28G06F111/08G06F113/08G06F119/14
CPCG06F30/28G06F2111/08G06F2113/08G06F2119/14
Inventor 陈江涛章超赵炜肖维赵娇吴晓军张培红肖中云杨福军崔鹏程刘深深李彬胡向鹏
Owner CALCULATION AERODYNAMICS INST CHINA AERODYNAMICS RES & DEV CENT
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