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:


Paper Publications

A Double-Passage Shape Correction Method for Predictions of Unsteady Flow and Aeroelasticity in Turbomachinery

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Affiliation of Author(s):航空宇航学院

Journal:ADVANCES IN APPLIED MATHEMATICS AND MECHANICS

Key Words:Double passage shape correction Fourier transformation unsteady flow aeroelasticity vibrating blades turbomachinery

Abstract:In this paper, a double-passage shape correction (DPSC) method is presented for simulation of unsteady flows around vibrating blades and aeroelastic prediction. Based on the idea of phase-lagged boundary conditions, the shape correction method was proposed aimed at efficiently dealing with unsteady flow problems in turbomachinery. However, the original single-passage shape correction (SPSC) may show the disadvantage of slow convergence of unsteady solutions and even produce nonphysical oscillation. The reason is found to be related with the disturbances on the circumferential boundaries that can not be damped by numerical schemes. To overcome these difficulties, the DPSC method is adopted here, in which the Fourier coefficients are computed from flow variables at implicit boundaries instead of circumferential boundaries in the SPSC method. This treatment actually reduces the interaction between the calculation of Fourier coefficients and the update of flow variables. Therefore a faster convergence speed could be achieved and also the solution stability is improved. The present method is developed to be suitable for viscous and turbulent flows. And for real three-dimensional (3D) problems, the rotating effects are also considered. For validation, a 2D oscillating turbine cascade, a 3D oscillating flat plate cascade and a 3D practical transonic fan rotor are investigated. Comparisons with experimental data or other solutions and relevant discussions are presented in detail. Numerical results show that the solution accuracy of DPSC method is favorable and at least comparable to the SPSC method. However, fewer iteration cycles are needed to get a converged and stable unsteady solution, which greatly improves the computational efficiency.

Volume:9

Issue:4

Page Number:839-860

ISSN No.:2070-0733

Translation or Not:no

Date of Publication:2017-08-01

Included Journals:SCIE

Correspondence Author:lzl

Pre One:An efficient predictor corrector-based dynamic mesh method for multi-block structured grid with extremely large deformation and its applications

Profile

    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)。