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| Numerical study of inflow equivalence ratio inhomogeneity on oblique detonation formation in hydrogen-air mixtures 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 71, 页码: 256-263 Authors: Fang YS(方宜申); Hu ZM(胡宗民); Teng HH(滕宏辉); Jiang ZL(姜宗林); Ng HD View  |  Adobe PDF(2663Kb)  |  Favorite  |  View/Download:363/92  |  Submit date:2018/02/08 Oblique Detonation Equivalence Ratio Mixture Inhomogeneity Detailed Chemistry |
| Uncertain reduced-order modeling for unsteady aerodynamics with interval parameters and its application on robust flutter boundary prediction 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 71, 页码: 214-230 Authors: Chen XJ; Qiu ZP; Wang XJ; Li YL; Wang RX(王睿星) Adobe PDF(4860Kb)  |  Favorite  |  View/Download:375/83  |  Submit date:2018/02/08 Uncertain Reduced-order Modeling Robust Flutter Analysis Interval Perturbation Method Uncertain Aeroelastic System |
| Aerodynamic measurement of a large aircraft model in hypersonic flow 期刊论文 CHINESE PHYSICS B, 2017, 卷号: 26, 期号: 11, 页码: 114702-1-114702-6 Authors: Meng BQ(孟宝清); Han GL(韩桂来); Zhang DL(张德良); Jiang ZL(姜宗林) Adobe PDF(4916Kb)  |  Favorite  |  View/Download:446/100  |  Submit date:2017/12/18 Hypersonic Aerodynamic Measurement Theoretical Study Vibration |
| 超声速三维进气道内激波干扰的研究 期刊论文 推进技术, 2017, 期号: 12, 页码: 6 Authors: 项高翔; 王春; 汪运鹏; 姜宗林 Adobe PDF(1393Kb)  |  Favorite  |  View/Download:454/90  |  Submit date:2017/12/22 高超声速流动 箱式进气道 侧壁压缩进气道 波系结构 流场区域 |
| 关于天飞行器若干重点问题的思考 科普文章 2017 Authors: 何郁依据网络资料撰写 Adobe PDF(4926Kb)  |  Favorite  |  View/Download:305/87  |  Submit date:2017/11/03 |
| On the response of coaxial surface thermocouples for transient aerodynamic heating measurements 期刊论文 EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2017, 卷号: 86, 页码: 141-148 Authors: Li JP(李进平); Chen H(陈宏); Zhang SZ(张仕忠); Zhang XY(张晓源); Yu HR(俞鸿儒); Chen, H (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China. Adobe PDF(1158Kb)  |  Favorite  |  View/Download:430/92  |  Submit date:2017/07/24 Heat Flux Measurement Thermocouple Response Characteristics Shock Tube |
| Experimental and Numerical Study on Hypersonic Flow over Double-Wedge Configuration 期刊论文 AIAA Journal, 2017, 卷号: 55, 期号: 9, 页码: 3227-3230 Authors: Meng BQ(孟宝清); Han GL(韩桂来); Yuan CK(苑朝凯); Wang C(王春); Jiang ZL(姜宗林) Adobe PDF(207Kb)  |  Favorite  |  View/Download:439/110  |  Submit date:2018/01/04 |
| 反压引起的带尖楔矩形隔离段流动分离迟滞现象实验研究 会议论文 中国航天第三专业信息网第三十八届技术交流会暨第二届空天动力联合会议, 中国辽宁大连, 2017-08-23 Authors: 黄庭隆; 岳连捷; 张新宇 Adobe PDF(1908Kb)  |  Favorite  |  View/Download:178/51  |  Submit date:2018/12/12 隔离段 反压 尖楔 分离区 流动分离 边界层分离 迟滞现象 激波串 纹影图像 |
| 关于Fotia隔离段流动突变理论分析的看法 会议论文 中国航天第三专业信息网第三十八届技术交流会暨第二届空天动力联合会议, 中国辽宁大连, 2017-08-23 Authors: 陈科挺; 岳连捷; 张新宇 Adobe PDF(623Kb)  |  Favorite  |  View/Download:346/48  |  Submit date:2018/12/12 隔离段 流动模型 出口 对外贸易 Fotia 核心流 |
| Numerical studies of static aeroelastic effects on grid fin aerodynamic performances 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2017, 卷号: 30, 期号: 4, 页码: 1300-1314 Authors: Huang CD(黄程德); Liu W(刘文); Yang GW(杨国伟) Adobe PDF(4021Kb)  |  Favorite  |  View/Download:323/97  |  Submit date:2017/11/29 Aeroelasticity Fluid-structure Interpolation Grid Fin Mesh Deformation Radial Basis Function |