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Reliability Providing Approach for Structurally- Parametrical Optimization Results of an “Aggressive” Intermediate Duct of the Bypass Gas-Turbine Engine

机译:可靠性提供结构上的旁路燃气涡轮发动机“侵蚀性”中间管道的结构 - 参数优化结果

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摘要

Limit assessment for the new optimization approach is carried out. This approach allows us to optimize the gas turbine duct elements by using the structural analysis and computational fluid dynamics methods, and to minimize the necessary number of CFD computations. Obtained results were verified and confirmed by experimental aerodynamic investigation.
机译:进行了新优化方法的限制评估。 该方法允许我们通过使用结构分析和计算流体动力学方法来优化燃气涡轮管道元件,并最小化必要的CFD计算数量。 通过实验空气动力学调查验证并确认获得的结果。

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