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A multi-fidelity framework for investigating the performance of super-cavitating hydrofoils under uncertain flow conditions

机译:一种多保真框架,用于在不确定流动条件下研究超空化水翼的性能

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Hydrofoils operating in a stable super-cavitating regime present great promise in designing high-performance marine vehicles with cruising speeds exceeding 100 knots. Due to the inherent complexity and multi-phase nature of the turbulent flow, assessing the performance of such hydrofoils for a wide range of operating conditions becomes a formidable task. Here we address this challenge by putting forth a data-driven multi-fidelity framework that is able to combine simplified computational models with a small number high-fidelity simulations and/or experimental data. The compositional synthesis of these variable fidelity information sources leads to significant computational expediency gains, and enables the construction of accurate predictive surrogates for a given hydrofoil performance metric. Using a Bayesian nonparametric approach based on Gaussian process priors, the resulting multi-fidelity surrogates can also naturally quantify uncertainty due to noisy or incomplete data. We demonstrate the effectiveness of the proposed framework by building stochastic response surfaces for the lift over drag ratio of a wedge-shaped super-cavitating hydrofoil operating in different flow regimes, as controlled by the angle of attack to the incoming flow and the cavitation index. In particular, we consider three information sources: 2D RANS simulations (low-fidelity), a 2D RANS solver corrected for spanwise effects through a reformulated lifting line theory (intermediate fidelity), and a fully 3D RANS solver (high-fidelity). We also show how noisy experimental data can be seamlessly incorporated in the workflow, and we validate our predictions against the cavitation tunnel experiments of Kermen et al.
机译:在稳定的超空穴制度中操作的水翼制品在设计高性能船用车辆时具有较高的承诺,巡航速度超过100节。由于湍流的固有复杂性和多相性质,评估这种水翼的性能对于各种操作条件变为强大的任务。在这里,我们通过提出数据驱动的多保真框架来解决这一挑战,该挑战能够将简化的计算模型与小数字高保真模拟和/或实验数据组合起来。这些可变保真信息源的组成合成导致显着的计算权宜之计,并且能够为给定的水翼艇性能度量进行准确的预测替代品。使用基于高斯过程前沿的贝叶斯非参数方法,所产生的多保真代理人也可以自然地量化由于嘈杂或不完整的数据而导致的不确定性。我们通过在不同流动方案中操作的楔形超空穴水翼膜的升降比率建设随机响应表面来证明所提出的框架的有效性,该架构在不同的流动方案中运行的楔形超空穴水翼仪的阻力比,如对进入流动的攻角和空化指数的控制。特别是,我们考虑三个信息来源:2D RANS模拟(低保真),通过重新改造的提升线理论(中间保真度)和完全3D RANS求解器(高保真)来校正跨翼效果的2D RAN求解器。我们还展示了如何在工作流程中无缝地纳入嘈杂的实验数据,我们验证了我们对Kermen等人的空化隧道实验的预测。

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