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Analysis of internally cooled structures using a higher order theory

机译:使用高阶理论分析内部冷却结构

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This paper presents the results of a study on the thermo-mechanical behavior of internally cooled silicon nitride structures. Silicon nitride is under consideration for elevated temperature aerospace engine applications, and techniques for lowering the operating temperature of structures composed of this material are under development. Lowering the operating temperature provides a large payoff in terms of fatigue life and may be accomplished through the use of thermal barrier coatings (TBCs) and the novel concept of included cooling channels. Herein, an in depth study is performed on the behavior of a flame-impinged silicon nitride plate with a TBC and internal channels cooled by forced air. The analysis is performed using the higher order theory for functionally graded materials (HOTFGM), which has been developed through NASA Glenn Research Center funding over the past several years. HOTFGM was chosen over the traditional finite element approach in order to facilitate examination of functionally graded silicon nitride structures for which HOTFGM is ideally suited. To accommodate the analysis requirements of the internally cooled plate problem, two crucial enhancements were made to the two-dimensional Cartesian-based version of HOTFGM, namely, incorporation of internal boundary capabilities and incorporation of convective boundary conditions. Results indicate the viability and large benefits of cooling the plate via forced air through cooling channels. Furthermore, cooling can positively impact the stress and displacement fields present in the plate, yielding an additional payoff in terms of fatigue life. Results illustrating the benefits associated with particular cooling channel arrangements and functionally grading the silicon nitride material are also presented. Finally, a spin off capability resulted from inclusion of internal boundaries Within HOTFGM; the ability to simulate the thermo-elastic response of structures with curved surfaces. This new capability is demonstrated, and through comparison with an analytical solution, shown to be viable and accurate.
机译:本文介绍了内部冷却的氮化硅结构的热机械行为的研究结果。氮化硅正在考虑用于高温航空发动机应用中,并且正在开发用于降低由这种材料构成的结构的工作温度的技术。降低工作温度可提供疲劳寿命方面的巨大回报,并且可以通过使用隔热涂层(TBC)和包括冷却通道的新颖概念来实现。在此,对具有TBC和通过强制空气冷却的内部通道的火焰冲击氮化硅板的性能进行了深入研究。使用高级功能梯度材料理论(HOTFGM)进行分析,该理论是在过去几年中通过NASA Glenn研究中心的资助开发的。选择HOTFGM而不是传统的有限元方法,以便于检查功能梯度材料最适合HOTFGM的氮化硅结构。为了适应内部冷却板问题的分析要求,对基于笛卡尔的二维HOTFGM版本进行了两个关键的改进,即合并了内部边界功能和合并了对流边界条件。结果表明,通过强制空气通过冷却通道对板进行冷却的可行性和巨大优势。此外,冷却可以对板中存在的应力和位移场产生积极影响,从而在疲劳寿命方面产生额外的收益。还提供了一些结果,这些结果说明了与特定冷却通道布置相关的好处,并在功能上分级了氮化硅材料。最后,剥离能力是由于在HOTFGM中包含内部边界而产生的;模拟具有弯曲表面的结构的热弹性响应的能力。通过与分析解决方案进行比较,证明了这种新功能的可行性和准确性。

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