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Numerical Investigation on Longitudinal Stage Separation of Spiked Two-Stage-to-Orbit Vehicle 期刊论文
Journal of Spacecraft and Rockets, 2023, 卷号: 60, 期号: 1, 页码: 215-229
作者:  Wang Y(王粤);  Wang YP(汪运鹏);  Wang C(王春);  Jiang ZL(姜宗林)
Adobe PDF(5479Kb)  |  收藏  |  浏览/下载：363/69  |  提交时间：2022/08/24
Multistage Launch Vehicle  Aerodynamic Characteristics  Shock Wave Interaction  Angle of Attack  Waverider  Boundary Layer Flow  Total Variation Diminishing  Adverse Pressure Gradient  Hypersonic Flows  Hypersonic Wind Tunnels  
Advances in Plasma Diagnostics and Applications 专著
Beijing:MDPI, 2022
作者:  Editors：Chen ZT;  Attri P;  Wang Q(汪球)
Adobe PDF(20682Kb)  |  收藏  |  浏览/下载：407/1  |  提交时间：2022/12/03
基于动态分区概念的高超声速燃烧大涡模拟 期刊论文
力学学报, 2022, 卷号: 54, 期号: 04, 页码: 954-974
作者:  姚卫;  刘杭;  张政;  肖雅彬;  岳连捷
Adobe PDF(1875Kb)  |  收藏  |  浏览/下载：263/61  |  提交时间：2022/06/10
高超声速燃烧  动态分区火焰面  分区自适应化学  分区并行自适应建表  改进延迟分离涡模拟  
Aerodynamic-Aeroacoustic Optimization of a Baseline Wing and Flap Configuration 期刊论文
APPLIED SCIENCES-BASEL, 2022, 卷号: 12, 期号: 3, 页码: 19
作者:  Ju SJ(鞠胜军);  Sun ZX(孙振旭);  Guo DL(郭迪龙);  Yang GW(杨国伟);  Wang YT(王业腾);  Yan C(闫畅)
Adobe PDF(12043Kb)  |  收藏  |  浏览/下载：258/35  |  提交时间：2022/03/28
high-lift devices  computational fluid dynamics  computational aeroacoustics  Kriging surrogate model  optimization design  
A Direct-Forcing Immersed Boundary Method for Incompressible Flows Based on Physics-Informed Neural Network 期刊论文
Fluids, 2022, 卷号: 7, 期号: 2, 页码: 56
作者:  Huang Y(黄毅);  Zhang ZY(张治愚);  Zhang X(张星)
Adobe PDF(6539Kb)  |  收藏  |  浏览/下载：356/82  |  提交时间：2022/01/27
physics-informed neural networks (PINN)  direct-forcing immersed boundary method  incompressible laminar flow  circular cylinder  
Gaseous Detonation Physics and Its Universal Framework Theory 专著
Beijing:Springer Nature, 2022
作者:  Jiang ZL(姜宗林);  Teng, Honghui
Adobe PDF(13641Kb)  |  收藏  |  浏览/下载：104/2  |  提交时间：2023/03/23
An optimized Eulerian-Lagrangian method for two-phase flow with coarse particles: Implementation in open-source field operation and manipulation, verification, and validation 期刊论文
PHYSICS OF FLUIDS, 2021, 卷号: 33, 期号: 11, 页码: 23
作者:  Zhang Y(张岩);  Lu XB(鲁晓兵);  Zhang XH(张旭辉)
Adobe PDF(3786Kb)  |  收藏  |  浏览/下载：350/70  |  提交时间：2022/01/13
Experimental study on shock wave control in high-enthalpy hypersonic flow by using SparkJet actuator 期刊论文
ACTA ASTRONAUTICA, 2021, 卷号: 188, 页码: 416-425
作者:  Xie, Wei;  Luo, Zhenbing;  Zhou, Yan;  Gao, Tianxiang;  Wu, Yun;  Wang Q(汪球)
Adobe PDF(8485Kb)  |  收藏  |  浏览/下载：115/57  |  提交时间：2022/10/25
SparkJet  High-enthalpy hypersonic flow  Shock control  Shock-on-shock interaction  Air supply  
Research on Critical Liquid-Carrying Model in Wellbore and Laboratory Experimental Verification 期刊论文
Processes, 2021, 卷号: 9, 页码: 923
作者:  Ke WQ(柯文琦);  Hou LT(侯林彤);  Wang LS(王黎松);  Niu J(牛骏);  Xu JY(许晶禹)
Adobe PDF(5284Kb)  |  收藏  |  浏览/下载：380/74  |  提交时间：2021/05/26
liquid loading  liquid-film reversal  critical liquid-carrying velocity  predictive model  
Reduction of surface friction drag in scramjet engine by boundary layer combustion 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 115, 页码: 106788
作者:  Xue, Rui;  Zheng, Xing;  Yue LJ(岳连捷);  Zhang, Qian;  He, Xin;  Yang, Jing;  Weng, Chao;  Li, Zhihao
Adobe PDF(5483Kb)  |  收藏  |  浏览/下载：124/41  |  提交时间：2022/10/25
Boundary layer combustion  Skin-friction reduction  Supersonic combustion  Scramjet engine