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个人信息Personal Information
教授 博士生导师
招生学科专业：
动力工程及工程热物理 -- 【招收硕士研究生】 -- 能源与动力学院
航空宇航科学与技术 -- 【招收博士、硕士研究生】 -- 能源与动力学院
能源动力 -- 【招收博士、硕士研究生】 -- 能源与动力学院
性别：男
毕业院校：南京航空航天大学
学历：南京航空航天大学
学位：工学博士学位
所在单位：能源与动力学院
办公地点：A10-640
联系方式：xie_wenzhong@126.com
电子邮箱：
扫描关注
- [1]Wenzhong Xie,Wei Yang.Prediction of self-starting limit of two-dimensional supersonic inlets considering viscous effect...:Aerospace science and technology
- [2]Wenzhong Xie,Yi Jin,Yan Ge,Shuzi Yang,Cheng Zeng,Shengmin Guo.Feasibility of employing the restarting process to evaluate the self-starting ability for hyperso...:Aerospace Science and Technology
- [3]谢文忠,Wenzhong Xie,Wu, Zhong-Ming,Yu, An-Yuan,Guo, Shengmin.Control of Severe Shock-Wave/Boundary-Layer Interactions in Hypersonic Inlets:JOURNAL OF PROPULSION AND POWER,2018
- [4]Wen-zhong Xie,Xiao-tian Gao,Xian Tang,Meng Huang,Shengmin Guo.Enlarged Self-Starting Operational Envelope for Hypersonic Inlets Using a Splitter:Journal of Aerospace Engineering
- [5]Wenzhong Xie,Yufen Wen,Shengmin Guo,Guangfu Ma,Hao Chen.Flow-Based Prediction for Self-Starting Limit of Two-Dimensional Hypersonic Inlets:Journal of Propulsion and Power
- [6]Wen-zhong Xie,Yan Ge,Hao Chen,Yu-fen Wen,Sheng-min Guo.Rapid supersonic performance prediction for 2D ramjet inlets:Aerospace Science & Technology
- [7]Wenzhong Xie,,Rongwei Guo.A Ventral Diverterless High Offset S-shaped Inlet at Transonic Speeds:CHINESE JOURNAL OF AERONAUTICS
- [8]Ge, Yan,谢文忠,Wenzhong Xie,Jing, Jian-Peng.Influence of internal contraction section configurations on self-starting ability of hypersonic i...:Hangkong Dongli Xuebao,2017
- [9]谢文忠,Wenzhong Xie,Ge, Yan,Zhao, Hao,Jing, Jianpeng.A test method for accelerating self-start of hypersonic inlets:Hangkong Dongli Xuebao,2018
- [10]谢文忠,Wenzhong Xie,Ma, Guangfu,Yu Lin,Jing, Jianpeng.Pseudo-shock characteristics in the two-dimensional supersonic inlet diffuser:Hangkong Dongli Xuebao,2017
- [11]葛严,,谢文忠,蔡建兵,蔡明先,黄兴.高速进气道出口快速撤锥再起动特性研究:推进技术
- [12]施欢,谢文忠,梁钢,金毅,靖建朋.不同边界层厚度下高马赫数进气道自起动过程研究:推进技术
- [13]谢文忠,高晓天,王肖,张德平.隔板对二元高马赫数进气道自起动性能的影响:推进技术
- [14]王肖,谢文忠,阳未,张德平.内收缩段泄流对超声速进气道的影响研究:推进技术
- [15]吴中明,谢文忠,张德平,王肖.隔板对低外阻二元高马赫数进气道反压特性的影响:推进技术
- [16]谢文忠,,葛严,赵昊,靖建朋.一种高超声速进气道加速自起动的实验方法:航空动力学报,2018
- [17]林宇,谢文忠,,张德平,高晓天.不起动流场对超声速/高超声速进气道自起动性能的影响:航空动力学报,2018
- [18]谢文忠,,葛严,靖建朋,林宇.内压缩段构型对高超声速进气道自起动性能的影响:航空动力学报,2017
- [19]谢文忠,,马广甫,林宇,靖建朋.二元超声速进气道扩张段内伪激波特性:航空动力学报,2017
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