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Numerical investigation of free oblique detonation wave induced by non-intrusive energy deposition 期刊论文
AIP ADVANCES, 2021, 卷号: 11, 期号: 12, 页码: 17
作者:  Zhang WS(张文硕);  Zhang, Zijian;  Jiang ZL(姜宗林);  Han X(韩信);  Liu, Yunfeng;  Wang, Chun
Adobe PDF(15045Kb)  |  收藏  |  浏览/下载：235/22  |  提交时间：2022/01/24
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  
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)  
Evolution of heat transfer at the stagnation point during the detached bow shock establishment 期刊论文
SHOCK WAVES, 2021, 页码: 8
作者:  Wang Q(汪球);  Li JP(李进平);  Luo K(罗凯);  Li JW(栗继伟);  Zhao W(赵伟)
Adobe PDF(1158Kb)  |  收藏  |  浏览/下载：241/50  |  提交时间：2021/05/17
Hypersonic  Aerodynamic heating  Detached bow shock  Shock tube  expansion tube  
Criteria for hypersonic airbreathing propulsion and its experimental verification 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
作者:  Jiang ZL(姜宗林);  Zhang ZJ(张子健);  Liu YF(刘云峰);  Wang C(王春);  Luo ZT(罗长童)
Adobe PDF(1806Kb)  |  收藏  |  浏览/下载：278/54  |  提交时间：2021/05/17
Concept demonstration  Hypersonic propulsion  Oblique detonation engine  Scramjet  Shock wave  Supersonic combustion  Wind tunnel test  
Noise reduction for temperature-sensitive paint measurement contaminated by strong background radiation in a high enthalpy hypersonic tunnel 期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 7
作者:  Peng, Di;  Liu, Xu;  Jiao, Lingrui;  Li, Ziyan;  Wen, Xin;  Yuan CK(苑朝凯);  Han GL(韩桂来);  Liu YF(刘云峰);  Liu, Yingzheng;  Jiang ZL(姜宗林)
Adobe PDF(3477Kb)  |  收藏  |  浏览/下载：246/46  |  提交时间：2021/03/30
Temperature-sensitive paint  Time-resolved measurement  Hypersonic flow  Background radiation  
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  
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：377/61  |  提交时间：2021/03/03
Unsteady pressure measurement  Pressure sensor  Pressure transmission tube  Dynamic response  Compressible flow  
Formation of stabilized oblique detonation waves in a combustor 期刊论文
COMBUSTION AND FLAME, 2021, 卷号: 223, 页码: 423-436
作者:  Zhang ZJ(张子健);  Wen, Chihyung;  Zhang WS(张文硕);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
Adobe PDF(3599Kb)  |  收藏  |  浏览/下载：327/89  |  提交时间：2021/03/03
Oblique detonation wave  Combustor  Oblique detonation engine  Normal detonation wave  Boundary layer separation