Building-Block-Flow Model for Large-Eddy Simulation

用于大涡模拟的积木流模型

• 批准号: 2317254
• 负责人: Adrian Lozano-Duran
• 金额: $ 32万
• 依托单位: Massachusetts Institute of Technology
• 依托单位国家: 美国
• 项目类别: Standard Grant
• 财政年份: 2023
• 资助国家: 美国
• 起止时间: 2023-06-15 至 2026-05-31
• 项目状态: 未结题
• 来源: https://www.nsf.gov/awardsearch/showAward?AWD_ID=2317254&HistoricalAwards=false
• 关键词: Building; Block; Flow; Model; Large

Computational fluid dynamics stands as an essential tool for the design and optimization of aerodynamic/hydrodynamic vehicles. It is estimated that the impact of reducing transportation drag by 5% would be equivalent to that of doubling the US wind energy production. However, computational predictions of fluid flows around realistic vehicles poses a unique challenge due to the ubiquity of complex flow physics, including adverse pressure-gradient effects, flow separation, and laminar-to-turbulent transition. While some computational models predict one or two scenarios, no model performs accurately across all flow phenomena. This project will seek to devise a unified closure model for computational fluid dynamics capable of accounting for a rich collection of flow physics. The goals of this project are to couple fundamental physics and machine-learning modeling for a new computational fluids model. The project also leverages existing programs to promote diversity and inclusion in engineering, including participation in annual summer research programs and undergraduate research opportunities to engage women and underrepresented minorities.The core assumption of the closure model proposed is that a finite set of simple canonical flows contains the essential physics to predict more complex scenarios. The approach is implemented using artificial neural networks with large-eddy simulation and brings together five unique advances: (1) the model is directly applicable to arbitrary complex geometries, (2) it is constructed to predict different flow regimes (zero/favorable/adverse mean-pressure-gradient wall turbulence, separation, statistically unsteady turbulence with mean-flow three-dimensionality, and laminar flow), (3) the model can be scaled-up to capture additional flow physics if needed (e.g., shock waves), (4) the model guarantees consistency with the numerical discretization and the gridding strategy by compensating for numerical errors, and (5) the output of the model is accompanied by a confidence score in the prediction used for uncertainty quantification and grid refinement. The cases of study range from canonical flat plate turbulence to complex flows such as realistic aircraft configurations. The foundations established in this work will enable new venues to model multiple flow regimes in computational fluid dynamics.This award reflects NSF's statutory mission and has been deemed worthy of support through evaluation using the Foundation's intellectual merit and broader impacts review criteria.

计算流体动力学是空气动力/流体动力飞行器设计和优化的重要工具。据估计，减少5%的运输阻力的影响将相当于美国风能产量翻一番。然而，由于复杂的流动物理现象的普遍存在，包括不利的压力梯度效应，流动分离，层流到湍流过渡，现实车辆周围的流体流动的计算预测提出了一个独特的挑战。虽然一些计算模型预测一个或两个场景，没有模型准确地执行所有的流动现象。这个项目将寻求为计算流体力学设计一个统一的封闭模型，能够解释丰富的流动物理学。该项目的目标是将基础物理和机器学习建模结合起来，构建新的计算流体模型。该项目还利用现有的计划，以促进工程的多样性和包容性，包括在每年的夏季研究计划和本科生的研究机会，让妇女和代表性不足的少数民族参与的参与。关闭模型的核心假设是，一个有限的简单规范流的集合包含基本的物理预测更复杂的情况。该方法使用具有大涡模拟的人工神经网络实现，并汇集了五个独特的进步：（1）该模型可直接应用于任意复杂的几何形状，（2）它被构造为预测不同的流态（零/有利/不利平均压力梯度壁湍流、分离、具有平均流三维性的统计非定常湍流和层流），（3）如果需要，模型可以按比例放大以捕获附加的流动物理（例如，冲击波），（4）该模型通过补偿数值误差来保证与数值离散化和网格化策略的一致性，以及（5）该模型的输出伴随有用于不确定性量化和网格细化的预测中的置信度得分。研究的情况范围从典型的平板湍流复杂的流动，如现实的飞机配置。在这项工作中建立的基础将使新的场地能够模拟计算流体力学中的多种流态。该奖项反映了NSF的法定使命，并通过使用基金会的知识价值和更广泛的影响审查标准进行评估，被认为值得支持。