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Application of a 2-D approximation technique for solving stress analyses problem in FEM

机译:二维逼近技术在有限元分析中的应用

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With the advent of computational techniques and methods like finite element method, complex engineering problems are no longer difficult to solve. These methods have helped engineers and designers to simulate and solve engineering problems in much more details than possible with experimental techniques. However, applying these techniques is not a simple task and require lots of acumen, understanding, and experience in obtaining a solution that is as close to an exact solution as possible with minimum computer resources. In this work using the finite element (FE) method, stress analyzes of the low-pressure turbine of a small turbofan engine is carried out by employing two different techniques. Initially, a complete solid model of the turbine is prepared which is then finite element modelled with the eight-node brick element. Stresses are calculated using this model. Subsequently, the same turbine is modelled with four-node shell element for calculation of stresses. Material properties, applied loads (inertial, aerodynamic, and thermal), and constraints were same for both the cases. Authors have developed a "2-D approximation technique" to approximate a 3-D problem into a 2-D problem to study the saving invaluable computational time and resources. In this statistics technique, the 3-D domain of variable thickness is divided into many small areas of constant thickness. It is ensured that the value of the thickness for each sub-area is the correct representative thickness of that sub area, and it is within three sigma limit. The results revealed that technique developed is accurate, less time consuming and computational effort saving; the stresses obtained by 2-D technique are within five percent of 3-D results. The solution is obtained in CPU time which is six times less than the 3-D model. Similarly, the number of nodes and elements are more than ten times less than that of the 3-D model. ANSYS ? was used in this work.
机译:随着诸如有限元法之类的计算技术和方法的出现,复杂的工程问题不再难于解决。这些方法已帮助工程师和设计人员比实验技术更详细地模拟和解决工程问题。但是,应用这些技术并不是一项简单的任务,需要大量的敏锐度,理解力和经验,才能以最少的计算机资源获得尽可能接近精确解决方案的解决方案。在这项使用有限元(FE)方法的工作中,采用两种不同的技术对小型涡扇发动机的低压涡轮进行了应力分析。最初,准备了涡轮机的完整实体模型,然后使用八节点砖单元对有限元进行建模。使用此模型计算应力。随后,使用四节点壳单元对同一涡轮进行建模,以计算应力。两种情况下的材料特性,施加的载荷(惯性,空气动力和热载荷)和约束条件相同。作者已经开发出一种“ 2-D近似技术”,可以将3-D问题近似为2-D问题,以研究节省的宝贵计算时间和资源。在这种统计技术中,可变厚度的3-D域被分为许多恒定厚度的小区域。确保每个子区域的厚度值是该子区域的正确代表厚度,并且在三个西格玛范围内。结果表明,所开发的技术准确,耗时少且节省了计算量; 2-D技术获得的应力在3-D结果的百分之五以内。该解决方案的CPU时间比3-D模型少六倍。同样,节点和元素的数量比3-D模型的数量少十倍以上。 ANSYS?用于这项工作。

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