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Automatic Generation of CFD-Ready Surface Triangulations from CAD Geometry

机译:从CAD几何图形自动生成CFD就绪的表面三角剖分

摘要

This paper presents an approach for the generation of closed manifold surface triangulations from CAD geometry. CAD parts and assemblies are used in their native format, without translation, and a part's native geometry engine is accessed through a modeler-independent application programming interface (API). In seeking a robust and fully automated procedure, the algorithm is based on a new physical space manifold triangulation technique which was developed to avoid robustness issues associated with poorly conditioned mappings. In addition, this approach avoids the usual ambiguities associated with floating-point predicate evaluation on constructed coordinate geometry in a mapped space, The technique is incremental, so that each new site improves the triangulation by some well defined quality measure. Sites are inserted using a variety of priority queues to ensure that new insertions will address the worst triangles first, As a result of this strategy, the algorithm will return its 'best' mesh for a given (prespecified) number of sites. Alternatively, the algorithm may be allowed to terminate naturally after achieving a prespecified measure of mesh quality. The resulting triangulations are 'CFD-ready' in that: (1) Edges match the underlying part model to within a specified tolerance. (2) Triangles on disjoint surfaces in close proximity have matching length-scales. (3) The algorithm produces a triangulation such that no angle is less than a given angle bound, alpha, or greater than Pi - 2alpha This result also sets bounds on the maximum vertex degree, triangle aspect-ratio and maximum stretching rate for the triangulation. In addition to tile output triangulations for a variety of CAD parts, tile discussion presents related theoretical results which assert the existence of such all angle bound, and demonstrate that maximum bounds of between 25 deg and 30 deg may be achieved in practice.
机译:本文提出了一种从CAD几何图形生成闭合歧管表面三角剖分的方法。 CAD零件和装配体以其原始格式使用,无需转换,并且零件的原始几何引擎可通过与建模者无关的应用程序编程接口(API)进行访问。在寻求鲁棒且完全自动化的过程时,该算法基于一种新的物理空间歧管三角测量技术,该技术被开发用来避免与条件差的映射有关的鲁棒性问题。此外,此方法避免了与在映射空间中构造的坐标几何上的浮点谓词评估相关的通常的歧义。该技术是渐进式的,因此每个新站点都通过一些定义明确的质量度量来改进三角剖分。使用各种优先级队列插入站点,以确保新插入将首先处理最差的三角形。作为此策略的结果,该算法将为给定(预定)数量的站点返回其“最佳”网格。可替代地,在实现对网格质量的预定量度之后,可以允许算法自然终止。产生的三角剖分是“ CFD就绪”的,因为:(1)边将基础零件模型匹配到指定的公差内。 (2)不相交的表面上非常接近的三角形具有匹配的长度比例。 (3)该算法生成三角剖分,以使角度不小于给定的角度边界,α或大于Pi-2alpha。此结果还为三角剖分的最大顶点度,三角形长宽比和最大拉伸率设置了边界。除了用于各种CAD零件的瓦片输出三角剖分之外,瓦片讨论还提供了相关的理论结果,这些结果断言了所有角度范围的存在,并证明了在实践中可以实现25度到30度之间的最大范围。

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