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Experimental Strain Measurements of Highly-Curved Blades

机译:高弯曲叶片的实验应变测量

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This paper presents an experimental-numerical investigation on the axial strain of highly-curved blades. Models of the blades were analyzed using a 2-D finite clement code, SectionBuilder, coupled with a comprehensive analysis code, Dymore, and first validated using strain measurements under a static tip load. Frequency responses were obtained under an impulsive load for each of the blades with multiple boundary conditions and compared with the numerical models. Experimental measurements under centrifugal loading from 0 up to 3300 RPM in a vacuum showed the effect of curvature on the axial strain, with significant bending strains observed in the responses for the curved blades that were also well captured by the numerical analysis. The present analysis shows that even moderate levels of out-of-plane curvature significantly increases the strain magnitudes, while higher levels of in-plane curvature have a much smaller impact.
机译:本文对高弯曲叶片的轴向应变进行了实验数值研究。使用2-D有限元素代码(SectionBuilder)和全面的分析代码(Dymore)来分析叶片的模型,并首先在静态叶尖载荷下使用应变测量对其进行验证。在具有多个边界条件的每个叶片的冲击载荷下获得了频率响应,并将其与数值模型进行了比较。在真空中从0到3300 RPM的离心载荷下的实验测量表明,曲率对轴向应变的影响,在弯曲叶片的响应中观察到了显着的弯曲应变,数值分析也很好地捕获了弯曲应变。目前的分析表明,即使适度的平面外曲率也会显着增加应变幅度,而较高的平面内曲率的影响则小得多。

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