Shi Zhiyu

Professor   Supervisor of Doctorate Candidates  

Gender:Male

Education Level:南京航空航天大学

Degree:Doctoral Degree in Engineering

School/Department:College of Aerospace Engineering

Discipline:Engineering Mechanics

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Paper Publications

A unified scaled boundary finite element method for transient two-dimensional vibro-acoustic analysis of plate-like structures

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Affiliation of Author(s):航空学院

Journal:COMPUTERS & STRUCTURES

Key Words:Vibro-acoustic analysis Time domain Unbounded domain Scaled boundary finite element method Doubly-asymptotic open boundary Spectral element

Abstract:This paper develops a unified and efficient simulation technique based on the scaled boundary finite element method (SBFEM) for transient structural-acoustic problems in two dimensions. The structural component can be an assembly of thin to moderately thick unidirectional plates. Each of them is treated as a plane strain problem and the principle of virtual work involving the inertial contribution is applied to derive the scaled boundary finite element equation. Only the longitudinal dimension is discretized with line elements and the solution through the thickness is expressed analytically as a Pade expansion. A variable transformation process together with certain structural assumptions leads to the static stiffness and mass matrices. The acoustic field can be a semi-infinite region, which is first divided by an artificial boundary into a near field and an exterior domain. The former is analyzed using the improved continued-fraction approach and the latter is modeled by the improved doubly-asymptotic open boundary. These formulations are based on velocity potential and established consistently in the SBFEM framework. High-order spectral elements are employed for both the structural and acoustic domains, to which independent discretization schemes are applied. Numerical examples are presented to demonstrate the excellent performances of the proposed technique. (C) 2018 Elsevier Ltd. All rights reserved.

ISSN No.:0045-7949

Translation or Not:no

Date of Publication:2018-06-01

Co-author:Liu, Lei

Correspondence Author:Shi Zhiyu

Pre One:Active double-panel sound insulation structure based on the active acoustical boundary acting on the boundaries of air gap sound field

Next One:Experimental study and finite element analysis of concrete-filled circular steel tubular K-type welded tube-gusset joints

Profile

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史治宇,男,汉族,教授、博士生导师。

1990年毕业于南京航空航天大学飞行器系,获得飞行器设计专业学士学位;1993年毕业于南京航空航天大学航空宇航学院,获得固体力学专业硕士学位;1996年毕业于南京航空航天大学航空宇航学院,获得固体力学专业博士学位。

1996年留校工作至今,2000年于南京航空航天大学航空宇航学院,晋升为副教授;2004年晋升为教授,2005年评为博士生导师。2008年被评为南京航空航天大学教学名师。

主要从事时变结构动力学及参数识别、结构声振耦合分析、结构有限元模型修正、结构健康监测与损伤诊断、动载荷识别、复合材料结构优化设计与分析等方面的研究工作。


发表学术论文,出版专著情况:

发表论文130多篇,爱思唯尔2021年和2022年中国高被引学者

出版《飞行器结构力学》和《变分原理及有限元》教材2本,其中《飞行器结构力学》被评选为“十三五”江苏省高等学校重点教材。


科研成果获奖及专利:

获省部级科技进步奖三等奖5次。

2018年获国家教学成果一等奖(排名第5);2017年获江苏省教学成果特等奖(排名第5)。


承担的科研项目情况:

主持完成国家自然科学基金面上项目3项、航空科学基金2项、江苏省自然科学基金面上项目1项,江苏省自然基金青年科技创新人才学术带头人项目1项,以及横向课题;参与完成国家自然科学基金重点项目1项。

正承担国家自然科学基金面上项目1项、国家重点研发计划项目子课题1项、以及多项横向课题。


备注:

欢迎报考力学博士、硕士研究生;航空宇航科学与技术硕士研究生;以及“机械”专业博士、硕士研究生!

邮箱:zyshi@nuaa.edu.cn; 手机:18914704215