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Simulation on Three-Dimensional Shock Interactions and Aerodynamic Heating Between Body and Wing 期刊论文
AIAA JOURNAL, 2021, 页码: 12
Authors:  Lin MY(林明月);  Wang C(王春);  Peng J(彭俊);  Jiang ZL(姜宗林)
Adobe PDF(4805Kb)  |  Favorite  |  View/Download：358/71  |  Submit date：2022/01/12
Characterizing combustion of a hybrid rocket using laser absorption spectroscopy 期刊论文
EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2021, 卷号: 127, 页码: 9
Authors:  Fang SH(方思晗);  Wang ZZ(王泽众);  Lin X(林鑫);  Li F(李飞);  Li RJ(李仁杰);  Li, Jing;  Zhang, Zhedian;  Liu, Yan;  Yu XL(余西龙)
Adobe PDF(4367Kb)  |  Favorite  |  View/Download：566/75  |  Submit date：2021/08/03
Tunable diode laser absorption spectroscopy  Hybrid rocket motor  Temperature  Partial pressure  Combustion efficiency  
Reconstructing shock front of unstable detonations based on multi-layer perceptron 期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 14
Authors:  Zhou, Lin;  Teng, Honghui;  Ng, Hoi Dick;  Yang PF(杨鹏飞);  Jiang ZL(姜宗林)
Adobe PDF(6382Kb)  |  Favorite  |  View/Download：257/42  |  Submit date：2021/11/01
Cellular detonation  Lead shock evolution  Multi-layer perceptron  Numerical simulations  
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
Authors:  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)  |  Favorite  |  View/Download：348/56  |  Submit date：2021/09/07
High mach number scramjet  Circular cross-section  TDLAS  Multi-view simultaneous imaging  POD  
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
Authors:  Tong XT(仝晓通);  Zhang QF(张启帆);  Yue LJ(岳连捷);  Zhang XY(张新宇)
Adobe PDF(8067Kb)  |  Favorite  |  View/Download：432/84  |  Submit date：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
Authors:  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)  |  Favorite  |  View/Download：401/95  |  Submit date：2021/03/03
Oblique detonation wave  Combustor  Oblique detonation engine  Normal detonation wave  Boundary layer separation