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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Affiliation of Author(s):航空学院
Journal:J Vib Shock
Abstract:Based on the active acoustical boundary method, an active double-panel sound insulation structure was presented, which consists of a double-panel structure and an active acoustical boundary arranged on the boundary of the air gap sound field. Simply supported panels were used to replace the active acoustical boundary and were acted by control forces. In the light of the acoustoelsticity theory, an analytical model was developed to calculate the optimal control forces, considering the minimum radiation sound power and minimum air gap sound power as the control targets. On the basis of the developed theoretical model, the sound transmission loss (STL) and responses of the subsystems of the active double-panel sound insulation structure were studied before and after control. Meanwhile, the effect of the dimensions of the active acoustical boundary on STL and responses of the subsystems were taken into account. The simulations carried out show that the active acoustical boundary control strategy can effectively improve the sound insulation performance of double-panel structures and the better control effect can be gotten with the target of minimum radiation sound power than that with the target of minimum air gap sound power. The active acoustical boundary has no influence on the vibration responses of the upper panel whilst the vibration responses of the lower panel and the air gap sound power are suppressed effectively. The active acoustical boundaries with different dimensions can all improve the sound insulation performance. Especially, in low frequency range, the same insulation performance can be gotten for the different dimensions, but in high frequency, range, the effect of the dimensions of active acoustical boundaries on the STL and responses of subsystems has no definite regularity, so the dimensions of the active acoustical boundaries can be optimized to improve the insulation performance in certain specific frequency ranges. © 2017, Editorial Office of Journal of Vibration and Shock. All right reserved.
ISSN No.:1000-3835
Translation or Not:no
Date of Publication:2017-11-15
Co-author:Ning, Shaowu,Xu, Xinyin
Correspondence Author:Ning, Shaowu,Shi Zhiyu
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。
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)。
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。
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