北京航空航天大学主页平台系统宋威--中文主页--论文

扫描手机二维码

欢迎您的访问
您是第位访客

开通时间：..

最后更新时间：..

登录| English | 手机版

同专业硕导

宋威赞
的个人主页 http://shi.buaa.edu.cn/songwei/zh_CN/index.htm
硕士生导师
主要任职：中国空气动力学会低跨超空气动力学专委会委员

论文当前位置：中文主页 >> 论文

[1] 宋威,艾邦成.多体空气动力学研究进展:力学学报,2022,54(6):1461-1484
[2] 宋威,艾邦成.多体分离动力学研究进展:航空学报,2022,43(9):025950
[3] Wei Song,Jingang Dong,Wei Lu,Zenghui Jiang.Trajectory and attitude deviations for internal store separation due to quasi-steady test method:Chinese Journal of Aeronautics,2022,35(2):74-81
[4] Peng Liao,Wei Song.Multi-fidelity convolutional neural network surrogate model for aerodynamic optimization based on transfer learning:Physics of Fluids,2021,33(127121)
[5] Wei Song,Bangcheng Ai.Analysis of aircraft-store compatibility for internal weapons separation:Aerospace Science and Technology,2021,110:106528
[6] Wei Song,Bangcheng Ai,Xiaojian Zhao,Zenghui Jiang,Wei Lu.Influence of control device on store separation from an open cavity:Aerospace Science and Technology,2020,106:106117
[7] Wei Song,Bangcheng Ai,Xiaojian Zhao.Prediction and evaluation on stage-separation compatibility of internally carried air-launch vehicle:Aerospace Science and Technology,2020,105(10600)
[8] .Aerodynamic Interference Reduction Using Aerospike for Two-stage Reusable Launch Vehicle:Journal of Aerospace Engineering,2023,36(4):06023002
[9] Peng Liao,Wei Song,Peng Du,Feng Feng,Yudong Zhang.Aerodynamic Intelligent Topology Design (AITD)-A Future Technology for Exploring the New Concept Configuration of Aircraft:aerospace,2023,10(46)
[10] 宋威,蒋增辉,贾区耀.细长锥边界层绊线转捩风洞自由飞试验:力学学报,2016,48(6):1301-1307

共27条 1/3

首页上页下页尾页页

版权所有 2014-2022 北京航空航天大学京ICP备05004617-3 文保网安备案号1101080018
地址：北京市海淀区学院路37号邮编：100191 电话：82317114