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| 激波风洞两级入轨飞行器纵向级间分离试验技术 期刊论文 航空学报, 2023, 卷号: 44, 期号: 17, 页码: 128126 Authors: 王粤; 汪运鹏; 姜宗林 Adobe PDF(6797Kb)  |  Favorite  |  View/Download:412/43  |  Submit date:2022/12/01 两级入轨 轨迹捕获 激波风洞 多体分离 动态试验 试验技术 |
| 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:337/94  |  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 |
| Divide and Conquer: A Quick Scheme for Symbolic Regression 期刊论文 INTERNATIONAL JOURNAL OF COMPUTATIONAL METHODS, 2022, 卷号: 19, 期号: 08, 页码: 25 Authors: Luo ZT(罗长童); Chen C(陈辰); Jiang ZL(姜宗林) Adobe PDF(204Kb)  |  Favorite  |  View/Download:187/40  |  Submit date:2023/02/07 Symbolic regression machine learning divide and conquer bi-correlation test mathematical modeling genetic programming |
| 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:128/2  |  Submit date:2023/03/23 |
| 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 Authors: 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)  |  Favorite  |  View/Download:294/64  |  Submit date:2021/05/17 Concept demonstration Hypersonic propulsion Oblique detonation engine Scramjet Shock wave Supersonic combustion Wind tunnel test |
| 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:356/178  |  Submit date:2021/03/30 High-enthalpy flow Hypersonic wind tunnel Aerospace vehicle Aerodynamic balance Heat flux sensor Optical measurement technique |
| On theory and methods for advanced detonation-driven hypervelocity shock tunnels 期刊论文 NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207 Authors: Jiang ZL(姜宗林); Li JP(李进平); Hu ZM(胡宗民); Liu YF(刘云峰); Yu HR(俞鸿儒) Adobe PDF(1090Kb)  |  Favorite  |  View/Download:278/101  |  Submit date:2020/11/30 hypervelocity shock tunnel detonation driver flight condition tailored condition test facilities |
| Application of CE/SE method to gas-particle two-phase detonations under an Eulerian-Lagrangian framework 期刊论文 JOURNAL OF COMPUTATIONAL PHYSICS, 2019, 卷号: 394, 页码: 18-40 Authors: Zhang ZJ(张子健); Wen CY; Liu YF(刘云峰); Zhang DL(张德良); Jiang ZL(姜宗林) View  |  Adobe PDF(4374Kb)  |  Favorite  |  View/Download:425/146  |  Submit date:2019/09/09 Two-phase detonation CE/SE Eulerian-Lagrangian MPI Aluminum-air detonation |
| Experimental investigation of liquid film cooling in hypersonic flow 期刊论文 PHYSICS OF FLUIDS, 2019, 卷号: 31, 期号: 4, 页码: 10 Authors: Yuan CK(苑朝凯); Li JP(李进平); Jiang ZL(姜宗林); Yu HR(俞鸿儒) View  |  Adobe PDF(4383Kb)  |  Favorite  |  View/Download:460/135  |  Submit date:2019/06/10 |
| Aerodynamic Testing at Duplicating Hypersonic Flight Conditions with Hyper-Dragon 会议论文 31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14 Authors: Jiang ZL(姜宗林); Yu HR(俞鸿儒) View  |  Adobe PDF(523Kb)  |  Favorite  |  View/Download:537/71  |  Submit date:2020/01/06 |