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Variable-state design parameters in the design of aero-structures made of intrinsically smart materials

机译：具有本质智能材料的航空结构设计中的可变状态设计参数

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The aerodynamic performance of aero-structures made of intrinsically smart materials, such as aeroelastic tailored wings and blades, cannot be obtained unless their material properties and structural characteristics are also known. The aerodynamic design of these structures is a naturally integrated design problem in which the set of design parameters comprises both aerodynamic and structural characteristics of the aero-structure. This paper references the inevitable problems arising when adopting an integrated design approach, suggesting an alternative approach for design of these structures. The concept of Variable State Design Parameters (VSDP) is introduced in this paper and it is explained how VSDP can be employed to convert the traditional integrated design process of intrinsically smart aero-structures, to a decoupled and hence computationally efficient design process. Through a design case study the practicality and efficiency of the new approach have been demonstrated.
机译：除非其材料性质和结构特征也是已知的，否则不能获得由本质上智能材料制成的空气结构的空气结构的空气动力学性能，例如空气弹性定制翅膀和叶片。这些结构的空气动力学设计是一种自然的集成设计问题，其中设计参数集包括空气结构的空气动力学和结构特征。本文参考采用集成设计方法时产生的不可避免的问题，旨在设计这些结构的替代方法。本文介绍了可变状态设计参数（VSDP）的概念，并说明了如何采用VSDP转换本质上智能航空结构的传统集成设计过程，以解耦并因此计算计算高效的设计过程。通过设计案例，研究了新方法的实用性和效率。

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