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| 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)![](/image/person.jpg)
Adobe PDF(9707Kb)  |   Favorite  |  View/Download:345/101  |  Submit date:2022/11/14 Two-stage to orbit Numerical simulation Stage separation Hypersonic flow Aerodynamic interference |
| 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)![](/image/person.jpg)
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 |
| Analytic investigation on error of heat flux measurement and data processing for large curvature models in hypersonic shock tunnels 期刊论文 APPLIED MATHEMATICS LETTERS, 2022, 卷号: 134, 页码: 8 Authors: Han GL(韩桂来) ; Qi L(齐力) ; Jiang ZL(姜宗林)![](/image/person.jpg)
Adobe PDF(1715Kb)  |   Favorite  |  View/Download:294/50  |  Submit date:2022/11/08 Heat flux Measurement Data processing Error Approximate solution |
| 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 |