Selected(0)Clear
Items/Page: Sort: |
| Effect of characteristic structure of nested composite hybrid rocket fuel grain on combustion properties 期刊论文 ACTA ASTRONAUTICA, 2024, 卷号: 218, 页码: 269-281 Authors: Wang, Ruoyan; Lin, Xin; Wang, Zezhong; Wu, Kun; Pan, Junjie; Zhang, Zelin; Luo, Jiaxiao; Li, Fei; Yu, Xilong Favorite  |  View/Download:4/0  |  Submit date:2024/05/21 Hybrid rocket Composite fuel grain Characteristic structure Radiation image Combustion properties |
| 基于多角度辐射成像的固液火箭发动机燃烧特性实验研究 学位论文 硕士论文,北京: 中国科学院大学, 2023 Authors: 罗家枭 Adobe PDF(6018Kb)  |  Favorite  |  View/Download:77/1  |  Submit date:2023/07/06 固液火箭发动机 燃烧特性 多角度辐射成像 模态分解方法 复合式燃料 |
| Flame Dynamics in the Combustion Chamber of Hybrid Rocket Using Multiangle Chemiluminescence 期刊论文 JOURNAL OF PROPULSION AND POWER, 2023 Authors: Luo JX(罗家枭); Zhang ZL(张泽林); Lin X(林鑫); Wang ZZ(王泽众); Wu K(吴坤); Zhou GX(周功喜); Zhang SH(张森豪); Li F(李飞); Yu XL(余西龙); Wu, Jie Adobe PDF(732Kb)  |  Favorite  |  View/Download:53/2  |  Submit date:2023/04/20 Combustion Instability Rayleigh Scattering Precombustion Chamber Hybrid Propellant Rocket Hybrid Rocket Motor Mass Flow Rate Convective Heat Transfer Characteristic Velocity Planar Laser Induced Fluorescence Propulsion and Power |
| Effects of swirl injection on the combustion of a novel composite hybrid rocket fuel grain 期刊论文 ACTA ASTRONAUTICA, 2022, 卷号: 199, 页码: 174-182 Authors: Zhang ZL(张泽林); Lin X(林鑫); Wang ZZ(王泽众); Wu K(吴坤); Luo JX(罗家枭); Fang SH(方思晗); Zhang CY(张春元); Li F(李飞); Yu XL(余西龙) Adobe PDF(9227Kb)  |  Favorite  |  View/Download:100/11  |  Submit date:2022/11/08 Hybrid rocket engine Swirl injection Novel composite fuel grain Regression rate Oxidizer-to-fuel ratio |
| Experimental Study of Combustion Characteristics of Micron-Sized Aluminum Particles and Liquid Water 期刊论文 JOURNAL OF PROPULSION AND POWER, 2022, 页码: 1-8 Authors: Ma P(马鹏); Wang SF(王双峰); Wang XZ(王秀珍) Adobe PDF(2629Kb)  |  Favorite  |  View/Download:200/44  |  Submit date:2022/03/25 |
| Gaseous Detonation Physics and Its Universal Framework Theory 专著 Beijing:Springer Nature, 2022 Authors: Jiang ZL(姜宗林); Teng, Honghui Adobe PDF(13641Kb)  |  Favorite  |  View/Download:113/2  |  Submit date:2023/03/23 |
| Determining the time-resolved mass flow rates of hybrid rocket fuels using laser absorption spectroscopy 期刊论文 ACTA ASTRONAUTICA, 2021, 卷号: 188, 页码: 110-120 Authors: Wang ZZ(王泽众); Lin X(林鑫); Li F(李飞); Peng JL(彭锦龙); Liu, Yan; Zhang ZL(张泽林); Fang SH(方思晗); Yu XL(余西龙) Adobe PDF(6496Kb)  |  Favorite  |  View/Download:301/57  |  Submit date:2021/11/01 Hybrid rocket engine Fuel mass flow rate Tunable diode laser absorption spectroscopy Temperature Partial pressure |
| Very high cycle fatigue (VHCF) response of additively manufactured materials: A review 期刊论文 FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES, 2021, 页码: 25 Authors: Caivano, Riccardo; Tridello, Andrea; Chiandussi, Giorgio; Qian GA(钱桂安); Paolino, Davide; Berto, Filippo Adobe PDF(26537Kb)  |  Favorite  |  View/Download:241/39  |  Submit date:2021/11/01 additive manufacturing (AM) aluminum alloy In718 Ti6Al4V very high cycle fatigue (VHCF) |
| Characterizing combustion of a hybrid rocket using laser absorption spectroscopy 期刊论文 EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2021, 卷号: 127, 页码: 9 Authors: Fang SH(方思晗); Wang ZZ(王泽众); Lin X(林鑫); Li F(李飞); Li RJ(李仁杰); Li, Jing; Zhang, Zhedian; Liu, Yan; Yu XL(余西龙) Adobe PDF(4367Kb)  |  Favorite  |  View/Download:535/66  |  Submit date:2021/08/03 Tunable diode laser absorption spectroscopy Hybrid rocket motor Temperature Partial pressure Combustion efficiency |
| Numerical and experimental study on high-speed hydrogen-oxygen combustion gas flow and aerodynamic heating characteristics 期刊论文 PHYSICS OF FLUIDS, 2021, 卷号: 33, 期号: 7, 页码: 11 Authors: Yu JP(于江鹏); Li JP(李进平); Wang Q(汪球); Zhang SZ(张仕忠); Zhang XY(张晓源) Adobe PDF(3271Kb)  |  Favorite  |  View/Download:250/48  |  Submit date:2021/11/01 |