Multi-disciplinary reliability optimized design method under condition of interval uncertainty based on sequential method
An uncertainty, optimization design technology, applied in the field of multidisciplinary reliability optimization design under the condition of interval uncertainty based on sequential method, to achieve the effect of improving computational efficiency
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Embodiment 1
[0045] In order to fully understand the characteristics of the invention and its applicability to engineering practice, this invention adopts a two-discipline coupling system for reliability optimization design, and compares the results obtained by the invention with those obtained by conventional reliability optimization design. The mathematical description of the present embodiment is as follows:
[0046]
[0047]Table 1 gives the uncertainty information of the input parameters in this embodiment, and the allowable reliability is set to 0.9
[0048] Table 1
[0049]
[0050] The specific results are shown in Table 2:
[0051] Table 2
[0052]
[0053] where N D is the number of optimization searches, N I is the number of uncertainty analysis, N R is the number of reliability analyzes.
[0054] It can be seen from Table 2 that the optimization results obtained by the proposed method of the present invention and the conventional reliability optimization design m...
Embodiment 2
[0056] In order to fully understand the characteristics of the invention and its applicability to engineering practice, a hypersonic wing multidisciplinary reliability optimization design problem is used to verify its effectiveness. Such as figure 2 The hypersonic wing shown is composed of beams, ribs, honeycomb sandwich and skin. The beams and ribs are made of titanium alloy materials, forming the basic frame of the wing. The titanium alloy skin covers the surface of the wing, and the honeycomb paper is filled between the skin, ribs and beams.
[0057] In this example, the thickness of ribs and beams (L rib , L beam ) is a design variable and also an uncertain variable, the elastic modulus E of titanium alloy T and allowable maximum displacement d allowable is an uncertain variable. The reliability constraint is: η(dis max ≤dis allowable )≥0.99. The optimization goal is to minimize the wing weight. The description of uncertain variables is shown in Table 3:
[0058...
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