DALIAN UNIVERSITY OF TECHNOLOGY
Login
中文
Home
Scientific Research
Research Projects
Published Books
Patents
Paper Publications
Research Field
Teaching Research
Teaching Achievement
Teaching Information
Teaching Resources
Awards and Honours
Other Rewards
Academic Honor
Scientific Awards
Enrollment Information
Student Information
My Album
Blog
Current position:
Home
>>
Scientific Research
Wei Qian
Personal Information
Professor Supervisor of Doctorate Candidates Supervisor of Master's Candidates
Scientific Research
Research Field
No content
Paper Publication...
More>>
侯良学, 张戈, 刘南, 王冬, 钱卫, 杨希明.基于风洞试验模型的跨声速颤振研究[J],振动与冲击,2019,38(13):236-241,260
李盼, 杨睿, 任宗金, 钱卫, Yang, Rui(yangrui@dlut.edu.cn).全动舵面载荷测量的压电天平设计与误差分析[J],哈尔滨工业大学学报,2018,50(1):181-185
白瑜光, 张有为, 钱卫, 陈香言.高温作用下飞行器舱体的动力学特性分析[J],应用基础与工程科学学报,2017,25(6):1170-1182
Yan Z., Qian W., Yang R., Sheng X..The manufacture and application for composites aeroelastic model of civil airliner wing in FL-26 transonic wind-tunnel[A],2016
Bai Y., Qian W..Influence of the rhomboid zone on aeroelastic experiments of supersonic aircraft[A],2016
Qian W., Bai Y., Wang D..Design, manufacture and frequency experiment of a novel flutter model for AGARD WING 445.6 with structure-similarity[A],2016
Patents
More>>
一种模拟全动舵面颤振模型弯扭支撑刚度的装置
一种用于超声速风洞全动舵面模型的多功能根肋
颤振风洞模型的全动舵面与弹性机身两铰点弹性连接系统
一种全动平尾跨音速颤振风洞试验模型方案
一种中央固支的后机身尾翼低速颤振模型
一种低超重比复合材料翼面颤振模型
Published Books
No content
Research Projects
数值飞行器原型系统的综合验证及应用, 国家科技部, 2016/07/14, 在研
高可扩展全耦合空气动力学数值模拟软件, 国家“863”项目, 2015/07/10, 结题
求解任意多重介质断裂问题的对偶界面积分边界元法研究, 国家自然科学基金项目, 2018/08/16-2022/04/18, 结题
考虑几何非线性的大展弦比机翼气动弹性模型加工, 企事业单位委托科技项目, 2014/11/10, 结题