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| Experimental Study of Longitudinal Stage Separation of Two-Body Configuration in Shock Tunnel 期刊论文
AIAA Journal, 2022, 卷号: 60, 期号: 12, 页码: 6940-6946
Authors: Wang Y(王粤) ; Wang YP(汪运鹏); Jiang ZL(姜宗林)
 Adobe PDF(2434Kb) |  Favorite | View/Download：338/95 | Submit date：2022/08/23
Aerodynamic Coefficients Two Stage to Orbit Aerodynamic Performance Hypersonic Flight Hypersonic Wind Tunnels Solenoid Valves Oblique Shock Pneumatic Actuator Hypersonic Flows Computer Aided Engineering |
| Gaseous Detonation Physics and Its Universal Framework Theory 专著
Beijing:Springer Nature, 2022
Authors: Jiang ZL(姜宗林); Teng, Honghui
Adobe PDF(13641Kb) | Favorite | View/Download：129/2 | Submit date：2023/03/23 |
| 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：348/68 | Submit date：2022/01/12 |
| 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
Authors: 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) | Favorite | View/Download：282/58 | Submit date：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
Authors: Yuan CK(苑朝凯); Jiang ZL(姜宗林)
Adobe PDF(3790Kb) | Favorite | View/Download：423/75 | Submit date：2021/03/03
Hypersonics Shock tunnels Flow characteristics |
| 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：383/94 | Submit date：2021/03/03
Oblique detonation wave Combustor Oblique detonation engine Normal detonation wave Boundary layer separation |
| Advances in critical technologies for hypersonic and high-enthalpy wind tunnel 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038
Authors: Jiang ZL(姜宗林); Hu ZM(胡宗民); Wang YP(汪运鹏); Han GL(韩桂来)
Adobe PDF(1129Kb) | Favorite | View/Download：357/178 | Submit date：2021/03/30
High-enthalpy flow Hypersonic wind tunnel Aerospace vehicle Aerodynamic balance Heat flux sensor Optical measurement technique |
| A Data-Correlation Model of Aerodynamic Heating Based on Globally Optimal Learning Method 会议论文
16th International Conference on Natural Computation, Fuzzy Systems and Knowledge Discovery (ICNC-FSKD 2020), 西安，中国, 19-21 December 2020
Authors: Chen Z(陈阵); Li S(李森); Luo ZT(罗长童); Jiang ZL(姜宗林)
Adobe PDF(1545Kb) | Favorite | View/Download：172/46 | Submit date：2021/02/01 |
| Intelligent Force-Measurement System Use in Shock Tunnel 期刊论文
SENSORS, 2020, 卷号: 20, 期号: 21, 页码: 6179
Authors: Wang YP(汪运鹏); Jiang ZL(姜宗林)
Adobe PDF(2149Kb) | Favorite | View/Download：203/59 | Submit date：2020/12/28
artificial intelligence BALANCE SYSTEM deep learning DESIGN dynamic calibration FLOWS force-measurement system strain-gauge balance |
| Impulse force-measurement system 期刊论文
SHOCK WAVES, 2020, 页码: 11
Authors: Wang YP(汪运鹏); Jiang ZL(姜宗林)
Adobe PDF(1551Kb) | Favorite | View/Download：281/85 | Submit date：2020/11/30
Shock tunnel High enthalpy Aerodynamic force measurement Strain gauge balance |
