The immersed interface method (IIM) for interfaces immersed in fluids

适用于浸没在流体中的界面的浸入界面法 (IIM)

• 批准号: 0915237
• 负责人: Sheng Xu
• 金额: $ 19.18万
• 依托单位: Southern Methodist University
• 依托单位国家: 美国
• 项目类别: Standard Grant
• 财政年份: 2009
• 资助国家: 美国
• 起止时间: 2009-07-01 至 2012-06-30
• 项目状态: 已结题
• 来源: https://www.nsf.gov/awardsearch/showAward?AWD_ID=0915237&HistoricalAwards=false
• 关键词: immersed; interface; method; IIM; interfaces

This award is funded under the American Recovery and Reinvestment Act of 2009 (Public Law 111-5).The key objective of this research is to combine the strength of the immersed interface method (IIM), hierarchical grids, and the level set method for accurate and and efficient simulation of interface problems.In particular, the investigator and his students develop the hierarchical-grid IIM for fluid-solid interfaces and the level set IIM for fluid-fluid interfaces. Hierarchical grids provide fine resolution for resolving flow and geometry at a solid and allow a large domain for treating open far-field boundary conditions. The hierarchical-grid IIM is particularly suitable for simulating nature's flyers or swimmers in moving frames. In the level set method, a fluid-fluid interface is captured as a level set of a scalar function which is evolved by a partial differential equation (PDE).The level set method is very robust for capturing interfaces subject to topological changes. Jump conditions occur at a fluid-fluid interface. They also appear at a fluid-solid interface when the solid is represented as a (singular) force concentrating at the interface through the delta function. The main idea of the IIM is to directly incorporate necessary jump conditions into a numerical scheme. How to achieve high accuracy if available jump conditions are limited?How to incorporate jump conditions if they are coupled? How to determine the force to enforce the motion of a moving rigid solid?In this research, the investigator and his students answer these questions. In particular, they apply generalized Taylor expansions to construct high-order finite differences with limited jump conditions, use augmented-variable approaches to implement coupled jump conditions, and develop a boundary condition capturing approach to model free-moving rigid objects. The intellectual merit of this research is reflected in three aspects: the comprehensive development and implementation of various numerical methods, the generation of new approaches for computational modeling of interfaces in fluids, and the extensibility of the ideas produced in this research to a broad range of other interface problems.Fluid-solid and fluid-fluid interface problems are very rich in nature and technological applications. Insect flight is a beautiful example of fluid-solid interface problems. Insect flight is fascinating not only because it is beautiful to human eyes but also because its unconventional aerodynamics has great technical importance, especially in helping design flapping-wing micro air vehicles (MAVs). One well-known example of fluid-fluid interface problems is in oil recovery. The idea is to push out the oil trapped in the ground by flooding with water. A technical problem for oil recovery is to find means to suppress the fingering instability at water-oil interfaces. To study such interface problems, computational fluid dynamics(CFD) has become a very important role. CFD can provide very detailed flow data, which are difficult or impossible to obtain experimentally. The CFD data help understand flow physics and help construct and validate reduced analytical models.Because of the variety of flows and associated complexity, development and improvement of CFD techniques is still in high demand. In this research, the investigator and his students develop CFD techniques to achieve high-fidelity simulation of various interface problems. They improve some existing CFD methods, combine the strength of each, and develop new ones.This research has impact on unveiling unconventional aerodynamics and hydrodynamics of nature's flyers and swimmers. It also has impact on lubricated transport, air-driven liquid cooling, and laser welding. Its educational impact includes: (1) blending research-related topics into existing and new curricula; (2) training graduate students for simulation-based research; and (3) engaging undergraduate students in the research. In particular, building a user input module for simulating nature's flyers and swimmers is a nice summer research opportunity for undergraduate students.

该奖项是根据2009年美国复苏和再投资法案资助的（公法111-5）。本研究的主要目标是联合收割机浸入界面法（IIM）、分层网格和水平集方法的优势，以准确有效地模拟界面问题。特别是，研究者和他的学生开发了流-固界面的层次网格IIM和流-流界面的水平集IIM。分层网格提供了很好的分辨率，解决流动和几何形状在一个固体，并允许一个大的域处理开放的远场边界条件。层次网格IIM特别适合于在移动帧中模拟自然界的飞行者或游泳者。在水平集方法中，流体-流体界面被捕获为由偏微分方程（PDE）演化的标量函数的水平集，对于捕获拓扑变化的界面具有很强的鲁棒性。跳跃条件发生在流体-流体界面处。当固体被表示为通过δ函数在界面处集中的（奇异）力时，它们也出现在流体-固体界面处。IIM的主要思想是直接将必要的跳跃条件纳入数值格式。如果可用的跳跃条件有限，如何实现高精度？如果跳跃条件是耦合的，如何合并它们？如何确定使运动的刚体运动的力？在这项研究中，研究者和他的学生回答了这些问题。特别是，他们应用广义泰勒展开来构造高阶有限差分有限跳跃条件，使用增广变量方法来实现耦合跳跃条件，并开发了一种边界条件捕获方法来模拟自由移动的刚性物体。本研究的学术价值体现在三个方面：各种数值方法的全面发展和实施，流体中界面计算建模的新方法的产生，以及本研究中产生的思想可扩展到广泛的其他界面问题。流-固和流-流界面问题在自然界和技术上都有非常丰富的应用。昆虫飞行是流固界面问题的一个很好的例子。昆虫飞行之所以迷人，不仅是因为它对人类的眼睛来说是美丽的，还因为它的非传统空气动力学具有巨大的技术重要性，特别是在帮助设计扑翼微型飞行器（MAVs）方面。流体-流体界面问题的一个众所周知的例子是在石油开采中。这个想法是通过注水来挤出困在地下的石油。抑制油水界面指进不稳定性是采油技术面临的一个技术难题。为了研究这类界面问题，计算流体动力学（CFD）已成为一个非常重要的角色。计算流体力学可以提供非常详细的流动数据，这些数据很难或不可能通过实验获得。CFD数据有助于理解流动物理学，并有助于构建和验证简化的分析模型。由于流动的多样性和相关的复杂性，CFD技术的发展和改进仍然是高需求。在这项研究中，研究者和他的学生开发CFD技术，以实现各种接口问题的高保真模拟。他们改进了现有的一些CFD方法，联合收割机结合各自的优势，并开发了新的方法。它还对润滑运输、空气驱动液体冷却和激光焊接产生影响。其教育影响包括：（1）将研究相关主题融入现有和新课程;（2）培训研究生进行基于模拟的研究;（3）让本科生参与研究。特别是，建立一个用户输入模块模拟自然的飞行员和游泳者是一个很好的夏季研究机会，为本科生。