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| 变时滞间隙非线性机翼颤振主动控制方法 期刊论文 北京航空航天大学学报, 2019, 卷号: 46, 期号: 10, 页码: 1899-1906 作者: 聂雪媛; 郑冠男; 杨国伟 Adobe PDF(1255Kb)  |  收藏  |  浏览/下载:244/42  |  提交时间:2020/11/18 颤振抑制 间隙非线性 时滞控制系统 状态观测 时变时延 |
| Kerosene-fueled supersonic combustion modeling based on skeletal mechanisms 期刊论文 ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 6, 页码: 1155-1177 作者: Yao W(姚卫) 浏览  |  Adobe PDF(9586Kb)  |  收藏  |  浏览/下载:643/293  |  提交时间:2019/12/17 Kerosene Supersonic combustion Large eddy simulation Skeletal mechanism Scramjet |
| 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 作者: 孟宇 Adobe PDF(11443Kb)  |  收藏  |  浏览/下载:678/44  |  提交时间: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 |
| Efficient strategy for reliability-based optimization design of multidisciplinary coupled system with interval parameters 期刊论文 APPLIED MATHEMATICAL MODELLING, 2019, 卷号: 75, 页码: 349-370 作者: Wang RX(王睿星); Luo Y 浏览  |  Adobe PDF(4483Kb)  |  收藏  |  浏览/下载:220/80  |  提交时间:2019/11/25 Multidisciplinary design optimization Non-probabilistic reliability Uncertainty propagation analysis Gradient information Interval reliability displacement |
| Numerical study of wedge-induced oblique detonations in unsteady flow 期刊论文 JOURNAL OF FLUID MECHANICS, 2019, 卷号: 876, 页码: 264-287 作者: Yang PF(杨鹏飞); Ng HD; Teng HH(滕宏辉) 浏览  |  Adobe PDF(1356Kb)  |  收藏  |  浏览/下载:357/120  |  提交时间:2019/09/09 detonations |
| DNS analysis of the effects of combustion on turbulence in a supersonic H2/air jet flow 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 93, 页码: 9 作者: Fu YW(符耀威); Yu ZP(于长平); Yan Z(闫正); Li XL(李新亮) 浏览  |  Adobe PDF(2894Kb)  |  收藏  |  浏览/下载:374/139  |  提交时间:2020/03/21 Supersonic combustion Turbulence jet Direct numerical simulations Coherent structures |
| Initiation of oblique detonation waves induced by a blunt wedge in stoichiometric hydrogen-air mixtures 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 92, 页码: 676-684 作者: Fang YS(方宜申); Zhang ZJ(张子健); Hu ZM(胡宗民); Deng, X 浏览  |  Adobe PDF(2321Kb)  |  收藏  |  浏览/下载:315/79  |  提交时间:2019/10/21 Oblique detonation wave Blunt wedge Initiation Hydrogen |
| Six sigma robust design optimization for thermal protection system of hypersonic vehicles based on successive response surface method 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2019, 卷号: 32, 期号: 9, 页码: 2095-2108 作者: Zhu JJ; Wang XJ; Zhang HG; Li YW; Wang RX(王睿星); Qiu ZP 浏览  |  Adobe PDF(2082Kb)  |  收藏  |  浏览/下载:418/189  |  提交时间:2020/03/21 Hypersonic vehicle Six sigma robust optimization Successive response surface Thermal protection system Uncertainty |
| 设计参数对幂次乘波体纵向静稳定性的影响 期刊论文 宇航学报, 2019, 期号: 08, 页码: 887-896 作者: 王晓朋; 张陈安; 刘文; 王发民; 叶正寅 浏览  |  Adobe PDF(663Kb)  |  收藏  |  浏览/下载:393/49  |  提交时间:2019/09/12 纵向静稳定性 幂次乘波体 高超声速滑翔飞行器 |
| Comparison of the reliability-based and safety factor methods for structural design 期刊论文 APPLIED MATHEMATICAL MODELLING, 2019, 卷号: 72, 页码: 68-84 作者: Wang XJ; Shi QH; Fan WC; Wang RX(王睿星); Wang L 浏览  |  Adobe PDF(1921Kb)  |  收藏  |  浏览/下载:346/74  |  提交时间:2019/09/09 Safety factor method Reliability-based design optimization Structural design Uncertainty |