已选(0)清除
条数/页: 排序方式: |
| Numerical simulation of hypersonic flat-plate boundary-layer blowing control 期刊论文 PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 12, 页码: 16 作者: Li ZX(李宗贤); Liu MK(刘美宽); Han GL(韩桂来); Wang DG(王大高); Jiang ZL(姜宗林) Adobe PDF(4748Kb)  |  收藏  |  浏览/下载:30/6  |  提交时间:2024/03/11 |
| Experimental demonstration of forced initiation of kerosene oblique detonation by an on-wedge trip in an ODE model 期刊论文 COMBUSTION AND FLAME, 2023, 卷号: 258, 页码: 6 作者: Han X(韩信); Liu YF(刘云峰); Zhang, Zijian; Zhang WS(张文硕); Yuan CK(苑朝凯); Han GL(韩桂来); Jiang ZL(姜宗林) Adobe PDF(1092Kb)  |  收藏  |  浏览/下载:70/4  |  提交时间:2023/11/28 |
| Standing oblique detonation for hypersonic propulsion: A review 期刊论文 PROGRESS IN AEROSPACE SCIENCES, 2023, 卷号: 143, 页码: 17 作者: Jiang ZL(姜宗林) Adobe PDF(10386Kb)  |  收藏  |  浏览/下载:29/1  |  提交时间:2024/02/26 Standing oblique detonation Scramjet engine Oblique detonation engine Shock wave Supersonic combustion Hypersonic ramjet propulsion |
| Characteristics of cellular structure of detonation waves propagating in annular channels 期刊论文 PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 10, 页码: 13 作者: Yao KP(姚克鹏); Yang PF(杨鹏飞); Wang C(王春); Jiang ZL(姜宗林) Adobe PDF(8005Kb)  |  收藏  |  浏览/下载:23/1  |  提交时间:2024/02/19 |
| 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 作者: 王粤; 汪运鹏; 姜宗林 Adobe PDF(6797Kb)  |  收藏  |  浏览/下载:340/35  |  提交时间: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 |
| Numerical investigation of unsteady aerodynamic characteristics induced by the interaction of oblique/bow shock waves during rotation 期刊论文 PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 8, 页码: 86124 作者: Wang DG(王大高); Han GL(韩桂来); Liu MK(刘美宽); Jiang ZL(姜宗林) Adobe PDF(10056Kb)  |  收藏  |  浏览/下载:48/0  |  提交时间:2023/09/26 |
| Force measurement using strain-gauge balance in shock tunnel based on deep learning 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 8, 页码: 43-53 作者: Nie SJ(聂少军); Wang YP(汪运鹏); Jiang ZL(姜宗林) Adobe PDF(2346Kb)  |  收藏  |  浏览/下载:20/2  |  提交时间:2024/02/26 Convolutional neural net-works Deep learning Frequency domain analysis Force measurement Time domain analysis Recurrent neural networks |
| Unsteady interaction mechanism of transverse stage separation in hypersonic flow for a two-stage-to-orbit vehicle 期刊论文 PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 5, 页码: 056120 作者: Wang Y(王粤); Wang YP(汪运鹏); Jiang ZL(姜宗林) Adobe PDF(9327Kb)  |  收藏  |  浏览/下载:188/61  |  提交时间:2023/05/26 Two-stage-to-orbit Hypersonic Numerical simulation Stage separation Aerodynamic interaction Unsteady flow Center of gravity |
| 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 作者: 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)  |  收藏  |  浏览/下载:68/2  |  提交时间:2023/06/15 |
| Numerical Investigation on Longitudinal Stage Separation of Spiked Two-Stage-to-Orbit Vehicle 期刊论文 Journal of Spacecraft and Rockets, 2023, 卷号: 60, 期号: 1, 页码: 215-229 作者: Wang Y(王粤); Wang YP(汪运鹏); Wang C(王春); Jiang ZL(姜宗林) Adobe PDF(5479Kb)  |  收藏  |  浏览/下载:363/69  |  提交时间:2022/08/24 Multistage Launch Vehicle Aerodynamic Characteristics Shock Wave Interaction Angle of Attack Waverider Boundary Layer Flow Total Variation Diminishing Adverse Pressure Gradient Hypersonic Flows Hypersonic Wind Tunnels |