气膜冷却孔几何形状的伴随优化

Fraser B. Jones, Todd A. Oliver, D. Bogard
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引用次数: 4

摘要

本文是关于气膜冷却优化方法的两篇系列论文的一部分,该系列论文旨在通过利用基于RANS的CFD的进步来快速优化气膜冷却孔几何形状,从而解决实验优化的局限性。在关于参数优化的论文[1]中,实验证明,与基准7-7-7孔相比,最优孔的空间平均效率提高了> 40%,并利用RANS作为实验数据的代理来开发。本文采用伴随优化方法设计了独特的气膜冷却孔几何形状。伴随优化超越了使用RANS作为实验数据的代理,而是利用RANS中可用的导数来充分优化形膜冷却孔的几何形状。经过实验验证,与基准7-7-7型井眼相比,最终的几何形状进一步提高了80%以上的性能。研究还表明,当扩大优化目标区域时,预计性能会进一步提高。此外,这些新的优化几何形状很容易通过增材制造(AM)工艺制造,并且比等效的参数优化孔形状消耗的时间要少得多。这些方法为充分利用AM提供的大设计空间提供了必要的工具,并将极大地改变膜冷却孔设计的未来。
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Adjoint Optimization of Film Cooling Hole Geometry
This paper is part of a two paper series on optimization methods for film cooling which seek to address the limitations of experimental optimization by utilizing advances in RANS based CFD to quickly optimize film cooling hole geometries. In the companion paper [1] on parametric optimization the optimum hole was experimentally demonstrated to have > 40% improvement in spatially averaged effectiveness compared to a baseline 7-7-7 hole, and was developed by leveraging RANS as a proxy for experimental data. In this paper adjoint based optimization was used to develop unique film cooling hole geometries. Adjoint optimization moves beyond using RANS as a proxy for experimental data instead utilizing the derivatives available in RANS to fully optimize the geometry of a shaped film cooling hole. The resulting geometry was experimentally validated to further increase performance by over 80% compared to the baseline 7-7-7 shaped hole. The study also show that further increases in performance are predicted when expanding the optimization target region. Furthermore, these new optimized geometries are readily manufactured by Additive Manufacturing (AM) processes and significantly less time consuming to generate than an equivalent parametrically optimized hole shape. These methods provide the tools necessary to fully utilize the large design space offered by AM and will be dramatically shift the future of film cooling hole design.
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