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Determining the time-resolved mass flow rates of hybrid rocket fuels using laser absorption spectroscopy 期刊论文
ACTA ASTRONAUTICA, 2021, 卷号: 188, 页码: 110-120
作者:  Wang ZZ(王泽众);  Lin X(林鑫);  Li F(李飞);  Peng JL(彭锦龙);  Liu, Yan;  Zhang ZL(张泽林);  Fang SH(方思晗);  Yu XL(余西龙)
Adobe PDF(6496Kb)  |  收藏  |  浏览/下载：275/50  |  提交时间：2021/11/01
Hybrid rocket engine  Fuel mass flow rate  Tunable diode laser absorption spectroscopy  Temperature  Partial pressure  
Hysteresis of Shock Train Movement in the Isolator with a Ramp 期刊论文
AIAA JOURNAL, 2021, 卷号: 59, 期号: 10, 页码: 3873-3882
作者:  Huang TL(黄庭隆);  Zhang QF(张启帆);  Yue LJ(岳连捷);  Zhang P;  Zhao QJ
Adobe PDF(2961Kb)  |  收藏  |  浏览/下载：204/42  |  提交时间：2022/02/17
Optical diagnostics in a detonation-driven direct-connected circular combustor fueled with hydrogen for mach 10 scramjet 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 54, 页码: 27801-27815
作者:  Zhou GX(周功喜);  Zhang X(张旭);  Li JP(李进平);  Zhang XY(张晓源);  Zhang SZ(张仕忠);  Lin X(林鑫);  Li F(李飞);  Chen H(陈宏);  Yue LJ(岳连捷);  Yu XL(余西龙)
Adobe PDF(4108Kb)  |  收藏  |  浏览/下载：329/47  |  提交时间：2021/09/07
High mach number scramjet  Circular cross-section  TDLAS  Multi-view simultaneous imaging  POD  
激波风洞高低压段钢膜片破裂特性研究 期刊论文
力学学报, 2021, 卷号: 53, 期号: 06, 页码: 1747-1757
作者:  聂少军;  汪运鹏;  薛晓鹏;  姜宗林
Adobe PDF(7665Kb)  |  收藏  |  浏览/下载：231/61  |  提交时间：2021/11/12
激波风洞  主膜片  爆轰驱动  破裂特性  数值模拟  
Laser ablation behavior of C/SiC composites subjected to transverse hypersonic airflow 期刊论文
CORROSION SCIENCE, 2021, 卷号: 183, 页码: 10
作者:  Wang Z(王哲);  Wang JT(王江涛);  Song HW(宋宏伟);  Yuan W(袁武);  Liu Yuwen;  Ma T(马特);  Huang CG(黄晨光)
Adobe PDF(5611Kb)  |  收藏  |  浏览/下载：428/94  |  提交时间：2021/05/06
Laser ablation (C)  C  SiC composite (A)  Hypersonic airflow (C)  Ablation morphology (C)  Mechanical erosion (C)  
Reconstruction model for heat release rate based on artificial neural network 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 37, 页码: 19599-19616
作者:  Li B(李波);  Yao W(姚卫);  Li YC(李亚超);  Fan XJ(范学军)
Adobe PDF(5169Kb)  |  收藏  |  浏览/下载：102/26  |  提交时间：2022/10/25
Heat release rate (HRR)  Artificial neural network (ANN)  Proper orthogonal -12omposition (POD)  Chemiluminescence  Supersonic hydrogen flame  
Instability mechanism and discharge regime diagnosis of microthrusters based on plasma properties 期刊论文
APPLIED OPTICS, 2021, 卷号: 60, 期号: 4, 页码: 1021-1030
作者:  Wang FY(王方仪);  Zhang SH(张少华);  Liu, Yan;  Yu XL(余西龙)
Adobe PDF(9020Kb)  |  收藏  |  浏览/下载：203/42  |  提交时间：2021/04/07
Experimental investigation of hypersonic flight-duplicated shock tunnel characteristics 期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 12
作者:  Yuan CK(苑朝凯);  Jiang ZL(姜宗林)
Adobe PDF(3790Kb)  |  收藏  |  浏览/下载：380/57  |  提交时间：2021/03/03
Hypersonics  Shock tunnels  Flow characteristics  
Influence of rectangular strips size on aerodynamic performance of a high-speed train subjected to crosswind 会议论文
Fluids Engineering Division Summer Meeting, FEDSM 2021, Virtual, Online, 10 August 2021 到 12 August 2021
作者:  Wang MY(王梦莹);  Sun ZX(孙振旭);  Ju SJ(鞠胜军);  Yang GW(杨国伟)
Adobe PDF(1369Kb)  |  收藏  |  浏览/下载：237/82  |  提交时间：2021/11/30
Aerodynamic performance  Crosswind  High-speed train  Orthogonal design  Rectangular strips  Variance analysis