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| Characteristics of cellular structure of detonation waves propagating in annular channels 期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 10, 页码: 13
Authors: Yao KP(姚克鹏) ; Yang PF(杨鹏飞); Wang C(王春); Jiang ZL(姜宗林)
 Adobe PDF(8005Kb) |  Favorite | View/Download：53/5 | Submit date：2024/02/19 |
| Optimal design of E-type coaxial thermocouples for transient heat measurements in shock tunnels 期刊论文
APPLIED THERMAL ENGINEERING, 2023, 卷号: 218, 页码: 11
Authors: Qi L(齐力); Han GL(韩桂来); Jiang ZL(姜宗林)
Adobe PDF(5274Kb) | Favorite | View/Download：213/11 | Submit date：2022/11/21
Coaxial thermocouples Lateral heat conduction Maximum temperature point Optimal design Numerical simulation |
| Numerical Investigation of Aerodynamic Separation Schemes for Two-Stage-to-Orbit-like Two-body System 期刊论文
Aerospace Science and Technology, 2022, 卷号: 131, 期号: Part A, 页码: 107995
Authors: Wang Y(王粤); Wang YP(汪运鹏); Jiang ZL(姜宗林)
Adobe PDF(9707Kb) | Favorite | View/Download：342/100 | Submit date：2022/11/14
Two-stage to orbit Numerical simulation Stage separation Hypersonic flow Aerodynamic interference |
| Theories and methods for designing hypersonic high-enthalpy flow nozzles 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 1, 页码: 318-339
Authors: Wang YP(汪运鹏); Jiang ZL(姜宗林)
Adobe PDF(2554Kb) | Favorite | View/Download：177/44 | Submit date：2022/06/10
Boundary layer correction High-enthalpy flow Hypersonic wind tunnel Nozzle design Real-gas effects |
| 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：245/39 | Submit date：2021/11/01
Cellular detonation Lead shock evolution Multi-layer perceptron Numerical simulations |
| 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 |
| Parameter-correlation study on shock-shock interaction using a machine learning method 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 107, 页码: 106247
Authors: Peng J(彭俊); Luo ZT(罗长童); Han ZJ(韩子健); Hu ZM(胡宗民); Han GL(韩桂来); Jiang ZL(姜宗林)
Adobe PDF(2818Kb) | Favorite | View/Download：320/120 | Submit date：2021/01/29
Shock-shock interaction Machine learning Hypersonic flow Impinging jet Genetic programming Triple point |
| 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：201/58 | Submit date：2020/12/28
artificial intelligence BALANCE SYSTEM deep learning DESIGN dynamic calibration FLOWS force-measurement system strain-gauge balance |
| Numerical investigation of a Mach 9 oblique detonation engine with fuel pre-injection 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 9
Authors: Zhang ZJ(张子健); Ma KF(马凯夫); Zhang WS(张文硕); Han X(韩鑫); Liu YF(刘云峰); Jiang ZL(姜宗林)
Adobe PDF(2608Kb) | Favorite | View/Download：277/119 | Submit date：2020/11/30
Oblique detonation engine Pre-injection Detonative combustion Mixing Hydrogen |
| Aerodynamic principles of shock-induced combustion ramjet engines 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 103, 页码: 8
Authors: Ma KF(马凯夫); Zhang ZJ(张子健); Liu YF(刘云峰); Jiang ZL(姜宗林)
Adobe PDF(1657Kb) | Favorite | View/Download：284/101 | Submit date：2020/08/26
Scramjet engines Shock-induced combustion ramjet engines Supersonic combustion Chapman-Jouguet detonation |
