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| 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 |
| A novel elastoplastic constitutive model for woven oxide/oxide ceramic matrix composites with anisotropic hardening 期刊论文 COMPOSITE STRUCTURES, 2019, 卷号: 229, 页码: UNSP 111420 作者: Liu H; Yang ZM(杨正茂); Yuan H 浏览  |  Adobe PDF(1701Kb)  |  收藏  |  浏览/下载:378/124  |  提交时间:2019/12/17 Oxide/oxide ceramic matrix composite Constitutive model Plastic potential function Anisotropic hardening Asymmetric tension and compression |
| 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:219/80  |  提交时间:2019/11/25 Multidisciplinary design optimization Non-probabilistic reliability Uncertainty propagation analysis Gradient information Interval reliability displacement |
| Experimental study of mode transition characteristics of a cavity-based scramjet combustor during acceleration 期刊论文 Aerospace Science and Technology, 2019, 卷号: 93, 期号: 10, 页码: UNSP 105316 作者: Meng Y(孟宇); Gu HB(顾洪斌); Zhuang JH(庄金衡); Sun WM(孙文明); Gao ZB(高占彪); Lian H(连欢); Yue LJ(岳连捷); Chang XY(张新宇) 浏览  |  Adobe PDF(3099Kb)  |  收藏  |  浏览/下载:361/94  |  提交时间:2019/10/15 Scramjet Combustor Mode Transition Liquid Kerosene Acceleration |
| 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:415/189  |  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 |
| 高速双锥绕流中热化学与输运模型影响研究 期刊论文 力学学报, 2019, 卷号: 51, 期号: 04, 页码: 1012-1021 作者: 丛彬彬; 万田 浏览  |  Adobe PDF(3373Kb)  |  收藏  |  浏览/下载:180/48  |  提交时间:2019/09/12 激波边界层相互作用 热化学非平衡 输运模型 双锥 |
| The Effects of Combustion on Turbulent Statistics in a Supersonic Turbulent Jet 期刊论文 ADVANCES IN APPLIED MATHEMATICS AND MECHANICS, 2019, 卷号: 11, 期号: 3, 页码: 664-674 作者: Fu YW(符耀威); Yu ZP(于长平); Yan Z(闫政); Li XL(李新亮) 浏览  |  Adobe PDF(82Kb)  |  收藏  |  浏览/下载:401/79  |  提交时间:2019/04/11 Supersonic jet turbulent combustion direct numerical simulation |
| A theoretical and computational study of the vibration excitation on the transition criteria of shock wave reflections 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 89, 页码: 299-306 作者: Peng J(彭俊); Zhang ZJ(张子健); Hu ZM(胡宗民); Jiang ZL(姜宗林) 浏览  |  Adobe PDF(2165Kb)  |  收藏  |  浏览/下载:393/92  |  提交时间:2019/09/09 Shock reflection Vibration excitation Mach reflection Transition criterion Hypersonic flow |