Selected(0)Clear
Items/Page: Sort: |
| 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 Adobe PDF(4250Kb)  |  Favorite  |  View/Download:261/4  |  Submit date:2022/07/08 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 Adobe PDF(6690Kb)  |  Favorite  |  View/Download:168/9  |  Submit date:2022/07/05 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 Adobe PDF(21257Kb)  |  Favorite  |  View/Download:820/32  |  Submit date:2021/06/07 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 Adobe PDF(11443Kb)  |  Favorite  |  View/Download:725/44  |  Submit date:2019/11/07 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 View  |  Adobe PDF(3578Kb)  |  Favorite  |  View/Download:523/134  |  Submit date:2018/10/30 |
| 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 Adobe PDF(10334Kb)  |  Favorite  |  View/Download:915/20  |  Submit date:2018/05/24 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. Adobe PDF(1329Kb)  |  Favorite  |  View/Download:637/124  |  Submit date:2017/03/28 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 Adobe PDF(1159Kb)  |  Favorite  |  View/Download:227/78  |  Submit date:2017/05/27 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 Adobe PDF(794Kb)  |  Favorite  |  View/Download:447/137  |  Submit date:2015/01/26 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 |