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| Standing oblique detonation for hypersonic propulsion: A review 期刊论文 PROGRESS IN AEROSPACE SCIENCES, 2023, 卷号: 143, 页码: 17 Authors: Jiang ZL(姜宗林)![](/image/person.jpg)
Adobe PDF(10386Kb)  |   Favorite  |  View/Download:65/7  |  Submit date:2024/02/26 Standing oblique detonation Scramjet engine Oblique detonation engine Shock wave Supersonic combustion Hypersonic ramjet propulsion |
| 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:289/47  |  Submit date:2022/11/08 Heat flux Measurement Data processing Error Approximate solution |
| Numerical investigation on the generation mechanism of aero-heating of rudder shaft from three-dimensional flow separation and vortices 期刊论文 AIP ADVANCES, 2022, 卷号: 12, 期号: 4, 页码: 13 Authors: Lin MY(林明月); Yang F(杨帆); Wang C(王春)![](/image/person.jpg)
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| 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)![](/image/person.jpg)
Adobe PDF(2554Kb)  |   Favorite  |  View/Download:175/44  |  Submit date:2022/06/10 Boundary layer correction High-enthalpy flow Hypersonic wind tunnel Nozzle design Real-gas effects |
| Experimental study on the evolution of mode waves in laminar boundary layer on a large-scale flat plate 期刊论文 PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 1, 页码: 16 Authors: Liu MK(刘美宽) ; Han GL(韩桂来) ; Jiang ZL(姜宗林)![](/image/person.jpg)
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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)![](/image/person.jpg)
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| 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)![](/image/person.jpg)
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)![](/image/person.jpg)
Adobe PDF(1090Kb)  |   Favorite  |  View/Download:277/101  |  Submit date:2020/11/30 hypervelocity shock tunnel detonation driver flight condition tailored condition test facilities |
| Numerical simulation of the interaction of two shear layers in double backward-facing steps 期刊论文 PHYSICS OF FLUIDS, 2019, 卷号: 31, 期号: 5, 页码: 15 Authors: Deng F(邓放); Han GL(韩桂来) ; Liu MK(刘美宽) ; Ding, J; Weng, PF; Jiang ZL(姜宗林)![](/image/person.jpg)
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