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Implementation of Transition Modeling for Analysis and Optimization of Two-Dimensional Airfoil Problems

机译:用于二维机翼问题分析和优化的过渡模型的实现

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This paper describes the implementation of various transition models used in conjunction with a single-equation turbulence model for predicting transitional flow over single and multiple element airfoil configurations. The analysis problem is formulated as well as the corresponding adjoint problem of the fully coupled flow-turbulence-transition equations. Test problems are shown for the computation of transitional airfoil cases, and the design optimization of a transitional airfoil using the adjoint-derived sensitivities is also demonstrated.
机译:本文介绍了与单方程湍流模型结合使用的各种过渡模型的实现,以预测单要素和多要素机翼构型的过渡流动。提出了分析问题以及完全耦合的流动湍流过渡方程的伴随问题。给出了计算过渡翼型情况的测试问题,并演示了使用伴随衍生的灵敏度对过渡翼型进行设计优化的方法。

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