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| Numerical Study on the Aerodynamic Heating Characteristics of the Cantilevered Injection System for Oblique Detonation Engine Inlets 期刊论文 AEROSPACE, 2023, 卷号: 10, 期号: 10, 页码: 18 Authors: Yang F(杨帆); Lin MY(林明月); Hu ZM(胡宗民); Han GL(韩桂来) Adobe PDF(8946Kb)  |  Favorite  |  View/Download:88/5  |  Submit date:2023/11/28 oblique detonation engine cantilevered injection localized high heat flux boundary layer separation reattachment |
| 气体动力学 专著 北京:科学出版社, 2023 Authors: 胡宗民; 姜宗林 Favorite  |  View/Download:72/0  |  Submit date:2024/01/11 |
| Transitional criterion and hysteresis of multiple shock-shock interference 期刊论文 PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 4, 页码: 46110 Authors: Lin MY(林明月); Yang F(杨帆); Hu ZM(胡宗民); Wang C(王春); Jiang ZL(姜宗林) Adobe PDF(5430Kb)  |  Favorite  |  View/Download:86/7  |  Submit date:2023/06/15 |
| Transitional wave configurations between Type III and Type IV oblique shock/bow shock interactions 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 3, 页码: 96-106 Authors: Peng J(彭俊); Li S(李帅); Yang F(杨帆); Lin MY(林明月); Han GL(韩桂来); Hu ZM(胡宗民) Adobe PDF(2838Kb)  |  Favorite  |  View/Download:63/3  |  Submit date:2023/04/20 Shock interactions Transitional configuration Aerodynamic heating Shear layer Mach interaction |
| 基于机器学习的高速飞行器双曲率前缘气动热预测方法 期刊论文 北京航空航天大学学报, 2023, 页码: 13 Authors: 杨帆; 林明月; 胡宗民; 罗长童 Adobe PDF(870Kb)  |  Favorite  |  View/Download:160/58  |  Submit date:2023/05/08 高超声速流动 气动热 多层分块算法 快速预测方法 驻点热流 双曲率前缘 |