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Detonation wave structure and thrust variation of a ram accelerator with different projectile velocities 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2023, 卷号: 143, 页码: 8
作者:  Shang JH(尚甲豪);  Wang, Kuanliang;  Wang, Aifeng;  Wang Q(汪球);  Zhao W(赵伟)
Adobe PDF(4127Kb)  |  收藏  |  浏览/下载：65/2  |  提交时间：2024/01/02
Ram accelerator  Detonation  Oblique detonation wave  Recirculation zone  
DeepStSNet: Reconstructing the quantum state-resolved thermochemical nonequilibrium flowfield using deep neural operator learning with scarce data 期刊论文
JOURNAL OF COMPUTATIONAL PHYSICS, 2023, 卷号: 491, 页码: 112344
作者:  Lv JQ(吕家琦);  Hong QZ(洪启臻);  Wang XY(王小永);  Mao, Zhiping;  Sun QH(孙泉华)
Adobe PDF(5558Kb)  |  收藏  |  浏览/下载：64/0  |  提交时间：2023/09/26
Hypersonic  Thermochemical nonequilibrium  State-to-state approach  Deep learning  Multiphysics  Data assimilation  
Study on initiation characteristics of oblique detonation induced by hydrogen jets in acetylene-air mixtures 期刊论文
FUEL, 2023, 卷号: 350, 页码: 128787
作者:  Yichen, Zhang;  Gaoxiang, Xiang;  Xiang, Gao;  Jia, Yu;  Xiquan, Hu;  Yirong, Xin;  Danyang, Li;  Wang Q(汪球)
Adobe PDF(8043Kb)  |  收藏  |  浏览/下载：182/2  |  提交时间：2023/07/17
Oblique detonation wave  Acetylene  Transverse jet  Numerical simulation  
Combustion Characteristics of a Swirl-Radial-Injection Composite Fuel Grain with Applications in Hybrid Rockets 期刊论文
AEROSPACE, 2023, 卷号: 10, 期号: 9, 页码: 19
作者:  Wang RY(王若岩);  Lin X(林鑫);  Wang ZZ(王泽众);  Wu K(吴坤);  Zhang ZL(张泽林);  Luo JX(罗家枭);  Li F(李飞);  Yu XL(余西龙)
Adobe PDF(8125Kb)  |  收藏  |  浏览/下载：77/2  |  提交时间：2023/10/30
hybrid rocket engine  swirl-radial injection  regression rate  flame images  combustion efficiency  
Numerical studies of flow patterns and fuel distribution of tandem-arranged multi jets in a hypersonic crossflow 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2023, 卷号: 139, 页码: 108383
作者:  Wang JL(王嘉麟);  Han GL(韩桂来)
Adobe PDF(5629Kb)  |  收藏  |  浏览/下载：47/0  |  提交时间：2023/07/17
Hypersonic flow  Tandem -arranged jets  Streamline pattern  Vortex structure  Fuel -air mixing  
Flame Dynamics in the Combustion Chamber of Hybrid Rocket Using Multiangle Chemiluminescence 期刊论文
JOURNAL OF PROPULSION AND POWER, 2023
作者:  Luo JX(罗家枭);  Zhang ZL(张泽林);  Lin X(林鑫);  Wang ZZ(王泽众);  Wu K(吴坤);  Zhou GX(周功喜);  Zhang SH(张森豪);  Li F(李飞);  Yu XL(余西龙);  Wu, Jie
Adobe PDF(732Kb)  |  收藏  |  浏览/下载：47/1  |  提交时间：2023/04/20
Combustion Instability  Rayleigh Scattering  Precombustion Chamber  Hybrid Propellant Rocket  Hybrid Rocket Motor  Mass Flow Rate  Convective Heat Transfer  Characteristic Velocity  Planar Laser Induced Fluorescence  Propulsion and Power  
乘波布局高超声速飞行器纵向静稳定特性分析 期刊论文
中国科学. 技术科学, 2014, 卷号: 44, 期号: 10, 页码: 1114-1122
作者:  贾子安;  张陈安;  王柯穆;  王发民
浏览  |  Adobe PDF(1111Kb)  |  收藏  |  浏览/下载：865/199  |  提交时间：2014/11/03
纵向静稳定性  乘波体  高超声速滑翔飞行器  气动力模型  
Discharge characteristics and abatement of volatile organic compounds using plasma reactor packed with ceramic Raschig rings 期刊论文
JOURNAL OF ELECTROSTATICS, 2013, 卷号: 71, 期号: 5, 页码: 939-944
作者:  Dou BJ;  Bin F(宾峰);  Wang C;  Jia QZ;  Li J;  Bin, F (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(833Kb)  |  收藏  |  浏览/下载：614/283  |  提交时间：2013/11/18
Non-thermal Plasmas  Lissajous Diagram  Discharge Parameters  Ceramic Raschig Rings  Toluene Removal