螺旋桨应力曲线有限元计算

J. H. Ma, W. C. Schnobrich, C. Stuber
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引用次数: 0

摘要

采用有限元位移模型对任意形状螺旋桨叶片在规定载荷作用下的弹性特性进行了预测。一般形式的固体元素被改编了。在单元空间中使用曲线坐标为定义复杂的设计曲面提供了一种实用的方法,也为应力计算提供了一种方便的方法。弯曲的三维单元很容易适应弯曲边界的弯曲几何,它们在螺旋桨问题中的应用简单而直接。由于曲面实体有限元的一般性质,计算结果收敛于真解,得到了较好的计算结果。从最近对全尺寸螺旋桨的分析中获得的高精度强烈表明,当前的发展代表了一种现实和可靠的方法来解决螺旋桨应力问题。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Propeller Stress Calculation Using Curved Finite Element
A finite element displacement model was utilized to predict the elastic behavior of a propeller blade having an arbitrary shape and subjected to prescribed loading. Solid elements in their general form were adapted. The use of curvilinear coordinates in element space provides a practical means for defining complex design surfaces and also provides an expedient method for stress calculations . The curved three-dimensional elements fit readily to a skewed geometry of curved boundary and their application to propeller problems is simple and straight-forward. The performance of the curved solid finite elements has been found to be excellent and the computed results, because of the general nature of the solid elements are assured to converge to the true solution . The high degree of accuracy obtained from a recent analysis of a full size propeller strongly suggests that the current development represents a realistic and reliable approach to the general solution of the propeller stress problem.
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