郭同庆
Professor Supervisor of Master's Candidates
Alma Mater:南京航空航天大学
Education Level:南京航空航天大学
Degree:Doctoral Degree in Engineering
School/Department:College of Aerospace Engineering
Discipline:Fluid Mechanics. Flight Vehicle Design
Business Address:C12-317
Contact Information:13915942440
E-Mail:
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Affiliation of Author(s):航空学院
Journal:JOURNAL OF COMPUTATIONAL PHYSICS
Key Words:Immersed boundary method Finite volume method Thermal flow Neumann boundary condition Preconditioned Navier-Stokes equations Fractional-step technique
Abstract:In the frameworks of immersed boundary method (IBM) and finite volume method (FVM), an implicit heat flux correction-based IB-FVM is proposed for thermal flows with Neumann boundary conditions. With the use of a fractional-step technique, the preconditioned Navier-Stokes (N-S) equations are solved by the FVM to obtain the intermediate solution in the prediction step and the heat flux is corrected by enforcing the Neumann condition in the correction step. Different from existing IBMs, the cell face centersare defined as the Eulerian points due to the heat flux computation at each face in the FVM. The Neumann condition is implemented in such a way that the interpolated temperature gradient is equal to the specified boundary value at the same point when the corrected gradient field is interpolated from the face centersto the Lagrangian points. To achieve an implicit algorithm, the temperature derivative corrections at the Lagrangian points are set as unknowns and a system of algebraic equations is established by constructing hybrid thin-plate splines (TPS) interpolation/delta function distribution. In the derivative interpolation process, the much more accurate TPS is introduced because the use of cosine delta function yields a less accurate solution. After the distribution process, the heat flux correction of a fluid cell is evaluated by using the solved temperature derivative corrections at the face centers, but that of a solid cell is calculated by using their additive inverses to supplement the same amount of heat flux into the solid domain as that flowing into the fluid domain across the boundary. Finally, the heat flux of a cell is corrected by adding the correction to the intermediate value and the corrected heat flux is utilized to solve the N-S equations in the prediction step. As compared with the available implicit IBMs for Neumann conditions, the present method avoids the introduction of auxiliary layers of Lagrangian points as well as the approximate conversion from the Neumann to Dirichlet condition and thus is suitable for an arbitrary geometry. The proposed method is verified by simulating several benchmark thermal flows with Neumann conditions, the natural convection in an annulus and the steady or unsteady forced convection over a stationary or oscillating cylinder. All the computed results agree well with the literature data. (C) 2019 Elsevier Inc. All rights reserved.
ISSN No.:0021-9991
Translation or Not:no
Date of Publication:2019-06-01
Co-author:Shen, Ennan,lzl,Wang, Yan,wy,Dong, Lu
Correspondence Author:lzl,gtq
长期从事计算流体力学、气动弹性力学和飞行器设计研究。首次提出工程急需的颤振余量变刚度分析技术,研发出系统成熟的飞行器静、动气动弹性CFD/CSD耦合算法和自主知识产权软件,广泛应用于型号工程。主持和参与国家自然基金、973计划、各种预研和型号攻关项目。发表学术论文40余篇,出版专著1部,授权发明专利3项;获江苏省优秀博士学位论文,工信部国防科技进步二等奖2项(本人分别排名第1、2),江苏省科学技术一等奖(本人排名第8)。