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| Coupling Effect of Multicavity on Flame Stabilization Mode Transitions in Scramjet Combustor 期刊论文 JOURNAL OF PROPULSION AND POWER, 2023 作者: Wu ZJ(吴振杰); Zhang QF(张启帆); Yu FY(于方游); Luo WH(罗苇航); Gao ZB(高占彪); Yue LJ(岳连捷) Adobe PDF(582Kb)  |  收藏  |  浏览/下载:45/0  |  提交时间:2023/06/15 Scramjet Engines Combustor Design flame stabilization mode transition path dependence |
| Optimal design of E-type coaxial thermocouples for transient heat measurements in shock tunnels 期刊论文 APPLIED THERMAL ENGINEERING, 2023, 卷号: 218, 页码: 11 作者: Qi L(齐力); Han GL(韩桂来); Jiang ZL(姜宗林) Adobe PDF(5274Kb)  |  收藏  |  浏览/下载:176/2  |  提交时间:2022/11/21 Coaxial thermocouples Lateral heat conduction Maximum temperature point Optimal design Numerical simulation |
| 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 作者: Wang YP(汪运鹏); Jiang ZL(姜宗林) Adobe PDF(2554Kb)  |  收藏  |  浏览/下载:140/27  |  提交时间:2022/06/10 Boundary layer correction High-enthalpy flow Hypersonic wind tunnel Nozzle design Real-gas effects |
| Design of a milli-newton force balance for hypersonic rarefied wind tunnel 期刊论文 MEASUREMENT, 2021, 卷号: 185, 页码: 7 作者: Wu CW(吴臣武); Liu C(刘聪); Hu DL(胡灯亮); Liu HL(刘宏立); Huang HJ(黄河激) Adobe PDF(4178Kb)  |  收藏  |  浏览/下载:282/66  |  提交时间:2021/11/15 Strain Balance Milli-newton Design Calibration |
| Intelligent Force-Measurement System Use in Shock Tunnel 期刊论文 SENSORS, 2020, 卷号: 20, 期号: 21, 页码: 6179 作者: Wang YP(汪运鹏); Jiang ZL(姜宗林) Adobe PDF(2149Kb)  |  收藏  |  浏览/下载:178/51  |  提交时间:2020/12/28 artificial intelligence BALANCE SYSTEM deep learning DESIGN dynamic calibration FLOWS force-measurement system strain-gauge balance |
| Thermodynamic optimization of Rankine cycle using CO2-based binary zeotropic mixture for ocean thermal energy conversion 期刊论文 APPLIED THERMAL ENGINEERING, 2020, 卷号: 178, 页码: 15 作者: Li CY; Pan LS(潘利生); Wang YZ Adobe PDF(2059Kb)  |  收藏  |  浏览/下载:274/126  |  提交时间:2020/08/26 OTEC (Ocean Thermal Energy Conversion) CO2-based mixture Performance evaluation Optimization design |
| Alleviation of lateral spillage of two-dimensional hypersonic inlet using waverider-configuration chines 期刊论文 INTERNATIONAL JOURNAL OF MODERN PHYSICS B, 2020, 卷号: 34, 期号: 14-16, 页码: 5 作者: Zhai J; Zhang CA(张陈安); Wang FM(王发民); Zhang WW Adobe PDF(510Kb)  |  收藏  |  浏览/下载:181/72  |  提交时间:2020/08/26 Hypersonic inlet lateral spillage waverider design method streamline tracing technology mass-flow ratio |
| Design methodology for shape transition inlets based on constant contraction of discrete streamtubes 期刊论文 PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2016, 卷号: 230, 期号: 8, 页码: 1496-1506 作者: Xiao YB(肖雅斌); Yue LJ(岳连捷); Ma SH; Zhang XY(张新宇); Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100864, Peoples R China. 浏览  |  Adobe PDF(1353Kb)  |  收藏  |  浏览/下载:398/91  |  提交时间:2016/09/14 Hypersonic Inlet Shape Transition Inward Turning Scramjet Design Method |
| 高压捕获翼位置设计方法研究 期刊论文 力学学报, 2016, 卷号: 48, 期号: 3, 页码: 576-584 作者: 李广利; 崔凯; 肖尧; 徐应洲 浏览  |  Adobe PDF(992Kb)  |  收藏  |  浏览/下载:408/63  |  提交时间:2016/12/16 High-speed Vehicles High Pressure Capturing Wing Uniform Experimental Design Polynomial Surrogate Model |
| 基于实验设计方法的高超声速飞机前缘型线优化分析 期刊论文 力学学报, 2016, 卷号: 48, 期号: 2, 页码: 290-299 作者: 胡守超; 崔凯; 李广利; 肖尧; 司徒明 浏览  |  Adobe PDF(1239Kb)  |  收藏  |  浏览/下载:339/63  |  提交时间:2016/12/16 Hypersonic Airplane Air-breathing Vehicle Shape Optimization Parameterization Uniform Design |