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LIMITATIONS TO FUNCTION STRUCTURES: A CASE STUDY IN MORPHING AIRFOIL DESIGN

机译:功能结构的局限性:以变形翼型设计为例的案例研究

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This paper presents an application of function structures in the design of single component morphing airfoils. A series of function structures are developed in an attempt to create an accurate model of a passively morphing airfoil. This paper describes each approach taken, while noting their modeling aspects that were successful or unsuccessful to identify representation features of existing function structure syntax and rules that relate to the usability of the models. System boundaries and definitions, function and flow definitions, carrier flows, and system state definitions are investigated. It was found that function structures in their current state, are incapable of accurately modeling the functionality of the shape changing aspect of a passively morphing airfoil. These limitations are identified and recommendations necessary to model artifacts similar to the morphing airfoil are presented. Finally, previous research efforts in the design of morphing airfoil technology are presented as solutions to certain key functions identified, thereby demonstrating the possible benefits of implementing function structures to this field.
机译:本文介绍了功能结构在单组分变形机翼设计中的应用。开发了一系列功能结构,以尝试创建被动变形机翼的精确模型。本文描述了所采用的每种方法,同时指出了其建模方面的成功或失败,以识别现有功能结构语法和与模型可用性相关的规则的表示特征。研究了系统边界和定义,功能和流定义,载流以及系统状态定义。已经发现,在其当前状态下的功能结构不能准确地对被动变形翼型的形状改变方面的功能进行建模。确定了这些局限性,并提出了对与变形机翼相似的伪影进行建模的必要建议。最后,介绍了变形翼型技术设计方面的先前研究成果,作为对某些关键功能的解决方案,从而证明了在该领域实施功能结构的潜在好处。

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