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高超声速 V 型前缘气动特性及流场作用机理研究 学位论文
硕士论文,北京: 中国科学院大学, 2022
Authors:  姜文清
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高超声速  V 形前缘  激波干扰  真实气体效应  
基于泛函学习的斜激波与弓形激波干扰规律研究 学位论文
硕士论文,北京: 中国科学院大学, 2022
Authors:  李帅
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激波干扰,高温气体效应,多层分块算法,高超声速流动,气动热  
强激波相互作用及其极端热载荷诱发机制研究 学位论文
博士论文,北京: 中国科学院大学, 2021
Authors:  彭俊
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高超声速  振动激发  激波反射  激波干扰  风洞实验  
超燃冲压发动机加速过程及等离子体对超声速火焰结构的影响 学位论文
博士论文,北京: 中国科学院大学, 2019
Authors:  孟宇
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超燃冲压发动机,燃烧模态,火焰结构,加速过程,微波,滑移电弧,等离子体  
Unsteady Aerodynamic Modeling Based on POD-ARX 期刊论文
INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING, 2018, 页码: 5902794
Authors:  Wang XP;  Zhang CA(张陈安);  Liu W(刘文);  Wang FM(王发民);  Ye ZY
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全乘波背部进气高超声速飞机新概念构型研究 学位论文
博士论文,北京: 中国科学院大学, 2018
Authors:  肖尧
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高超声速飞行器  乘波体  背部进气布局  升阻比  气动设计与优化  
Local Piston Theory with Viscous Correction and Its Application 期刊论文
AIAA Journal, 2017, 卷号: 55, 期号: 3, 页码: 942-954
Authors:  Liu W(刘文);  Zhang CA(张陈安);  Han HQ;  Wang FM(王发民);  Zhang, CA (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Hypersonic  Unsteady Aerodynamics  Piston Theory  Aeroelasticity  
Numerical simulation and wind tunnel testing of flutter about an all- Movable horizontal tail at transonic speeds 会议论文
29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014, St. Petersburg, Russia, September 7, 2014 - September 12, 2014
Authors:  Qian W;  Yang GW(杨国伟);  Zheng GN(郑冠男);  Zhang GJ
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All-movable Horizontal Tail  Flutter Boundaries  Overload Factors  Structure Dynamics  Transonic Flutter  Transonic Speed  Wind Tunnel Tests  Wind-tunnel Testing  
基于CFD气动力辨识模型的气动弹性数值计算 期刊论文
振动与冲击, 2014, 卷号: 33, 期号: 20, 页码: 20-25
Authors:  聂雪媛;  刘中玉;  杨国伟
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气动弹性  非定常气动力辨识  降阶模型  颤振  随机白噪声激励  
Fast Dynamic Mesh Method and its Application on Aeroelasticity 会议论文
7th Asian-Pacific Conference on Aerospace Technology and Science, 7th APCATS 2013, Taiwan, China, MAY 23-26, 2013
Authors:  Yang GW(杨国伟);  Zheng GN(郑冠男);  Nie XY(聂雪媛)
Adobe PDF(3458Kb)  |  Favorite  |  View/Download:686/242  |  Submit date:2014/03/11
Dynamic Mesh  Rbf  Reduced-point Option  Aeroelasticity