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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)
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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)
Adobe PDF(1715Kb) | Favorite | View/Download：273/42 | 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)
Adobe PDF(16512Kb) | Favorite | View/Download：177/27 | Submit date：2022/07/18 |
| 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：153/33 | 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)
Adobe PDF(5472Kb) | Favorite | View/Download：258/40 | Submit date：2022/03/05 |
| 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：322/58 | Submit date：2022/01/12 |
| 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：339/173 | 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：263/101 | 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)
 View | Adobe PDF(5760Kb) | Favorite | View/Download：551/86 | Submit date：2019/10/21 |
