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IDDES method based on differential Reynolds-stress model and its application in bluff body turbulent flows 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 119, 页码: 13
作者:  Wang, Gang;  Li, Quanzheng;  Liu Y(刘毅)
Adobe PDF(4661Kb)  |  收藏  |  浏览/下载:187/40  |  提交时间:2022/06/11
Detached-eddy simulation  Reynolds-stress model  Massively separated flows  Tandem cylinders  Launch vehicle  Transonic buffet  
Advances in plasma-assisted ignition and combustion for combustors of aerospace engines 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 27
作者:  Li, Mengzhe;  Wang, Zhikai;  Xu, Rongguang;  Zhang, Xiaoliang;  Chen, Zhitong;  Wang Q(汪球)
Adobe PDF(8841Kb)  |  收藏  |  浏览/下载:268/107  |  提交时间:2021/11/01
Non-equilibrium plasma  Plasma-assisted ignition  Plasma-assisted combustion  Aerospace engine  Combustor  Extreme condition  
Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 14
作者:  Yao W(姚卫);  Liu H(刘杭);  Yue LJ(岳连捷);  Xiao YB(肖雅彬)
Adobe PDF(2954Kb)  |  收藏  |  浏览/下载:262/58  |  提交时间:2021/11/15
Hypersonic combustion  Hydrogen  Improved Delayed Detached Eddy  Simulation (IDDES)  Dynamic zone flamelet model  Scramjet  
Longitudinal aerodynamic modeling and verification for air-launch-to-orbit system during stage separation 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 21
作者:  Yang L(杨磊);  Ye, Zhengyin;  Li WH(李文皓);  Sun QH(孙泉华)
Adobe PDF(4621Kb)  |  收藏  |  浏览/下载:254/52  |  提交时间:2021/11/01
Store separation  Aerodynamic modeling  Interference aerodynamics  Dynamic simulation  Air-launch-to-orbit  
Flow structure of pressure transmission tube and its influence on unsteady pressure measuring results in compressible flow 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 108, 页码: 22
作者:  Tong XT(仝晓通);  Zhang QF(张启帆);  Yue LJ(岳连捷);  Zhang XY(张新宇)
Adobe PDF(8067Kb)  |  收藏  |  浏览/下载:378/62  |  提交时间:2021/03/03
Unsteady pressure measurement  Pressure sensor  Pressure transmission tube  Dynamic response  Compressible flow  
Numerical investigation of a Mach 9 oblique detonation engine with fuel pre-injection 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 9
作者:  Zhang ZJ(张子健);  Ma KF(马凯夫);  Zhang WS(张文硕);  Han X(韩鑫);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
Adobe PDF(2608Kb)  |  收藏  |  浏览/下载:265/110  |  提交时间:2020/11/30
Oblique detonation engine  Pre-injection  Detonative combustion  Mixing  Hydrogen  
Effect of the fuel-air flow velocity on heat release rate of swirling non-premixed methane flames 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 95, 页码: UNSP 105465
作者:  Wang KL(王宽亮);  Li F(李飞);  Zou PF(邹鹏飞);  Lin X(林鑫);  Mao RH(毛荣海);  Yu XL(余西龙)
浏览  |  Adobe PDF(2678Kb)  |  收藏  |  浏览/下载:257/61  |  提交时间:2020/03/21
Swirl flame  Heat release  Chemiluminescence  3D-CTC  
Effect of the fuel-air flow velocity on heat release rate of swirling non-premixed methane flames 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 95, 页码: UNSP 105465
作者:  Wang KL(王宽亮);  Li F(李飞);  Zou PF(邹鹏飞);  Lin X(林鑫);  Mao RH(毛荣海);  Yu XL(余西龙)
浏览  |  Adobe PDF(2678Kb)  |  收藏  |  浏览/下载:202/67  |  提交时间:2020/03/21
Swirl flame  Heat release  Chemiluminescence  3D-CTC  
Experimental study of flame characteristics of ethylene and its mixture with methane and hydrogen in supersonic combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 86, 页码: 775-781
作者:  Zhong FQ(仲峰泉);  Cheng LW(程柳维);  Gu HB(顾洪斌);  Zhang XY(张新宇)
Adobe PDF(2032Kb)  |  收藏  |  浏览/下载:295/86  |  提交时间:2019/05/29
Supersonic combustor  Hydrocarbon  Mixture fuel  Flame structure  Ignition  
An efficient single-loop strategy for reliability-based multidisciplinary design optimization under non-probabilistic set theory 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 73, 页码: 148-163
作者:  Wang XJ;  Wang RX(王睿星);  Wang L;  Chen XJ;  Geng XY
浏览  |  Adobe PDF(3200Kb)  |  收藏  |  浏览/下载:478/106  |  提交时间:2018/10/30
Non-probabilistic reliability based  multidisciplinary design optimization  Single loop strategy  Uncertainty multidisciplinary analysis  Non-probabilistic reliability analysis  Translating distance calculation