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高超声速下三维侧压进气道激波干扰的研究 会议论文
中国航天第三专业信息网第三十七届技术交流会暨第一届空天动力联合会议, 中国陕西西安, 2016-08-17
Authors:  项高翔;  王春;  姜宗林
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高超声速流动  体-翼激波干扰  波系结构  流场区域  
Starting Process in a Large-Scale Shock Tunnel 会议论文
22nd AIAA Computational Fluid Dynamics Conference, Dallas, TX, JUN 22-26, 2015
Authors:  Wang YP;  Hu ZM(胡宗民);  Liu YF(刘云峰);  Jiang ZL(姜宗林);  Wang, YP (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
View  |  Adobe PDF(764Kb)  |  Favorite  |  View/Download：374/106  |  Submit date：2016/06/28
Role of wall temperature on shock train in a rectangular isolator 会议论文
52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016, Salt Lake City, UT, United states, July 25, 2016 - July 27, 2016
Authors:  Lu HB;  Wang D;  Chen X;  Yue LJ(岳连捷);  Ji, Feng (yuelj@imech.ac.cn)
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Aero  Heating  Dual Mechanisms  On Flow  Shock Train  Specific Heat Ratio  Total Pressure  Total Temperatures  Wall Temperatures  
Visualization of flow separation inside cut kerf during laser cutting of thick sections 会议论文
34th International Congress on Applications of Lasers and Electro-Optics (ICALEO), Atlanta, GA, OCT 18-22, 2015
Authors:  Zhang C;  Wen P;  Yao ZH;  Yuan YM(袁越明);  Fan XJ(范学军);  Wen, P (reprint author), Tsinghua Univ, State Key Lab Tribol, Beijing 100084, Peoples R China.
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