机构

• 力学研究所 [13]

采集方式

• OAI收割 [13]

内容类型

• 期刊论文 [12]
• 会议论文 [1]

发表日期

• 2024 [3]
• 2023 [4]
• 2022 [2]
• 2021 [2]
• 2020 [2]

学科主题

• Engineerin... [1]
• Materials ... [1]

筛选

浏览/检索结果: 共13条，第1-10条 帮助 条数/页： 5101520253035404550556065707580859095100 排序方式： 请选择题名升序题名降序提交时间升序提交时间降序作者升序作者降序发表日期升序发表日期降序 Effect of characteristic structure of nested composite hybrid rocket fuel grain on combustion properties 期刊论文  OAI收割 ACTA ASTRONAUTICA, 2024, 卷号: 218, 页码: 269-281 作者:  Wang, Ruoyan;  Lin, Xin;  Wang, Zezhong;  Wu, Kun;  Pan, Junjie   |  收藏  |  浏览/下载：33/0  |  提交时间：2024/05/21 Hybrid rocket  Composite fuel grain  Characteristic structure  Radiation image  Combustion properties   Superior Al90Mg10-Based Composite Fuel Grain for a Hybrid Rocket Engine 期刊论文  OAI收割 JOURNAL OF SPACECRAFT AND ROCKETS, 2024, 页码: 9 作者:  Wang, Zezhong;  Lin, Xin;  Pan, Junjie;  Luo, Jiaxiao;  Wang, Ruoyan   |  收藏  |  浏览/下载：46/0  |  提交时间：2024/05/21 Combustion Efficiency  Emission Spectroscopy  Hybrid Rocket Engines  Paraffin Based Fuels  Regression rate  Aluminium Alloys  3D Printing   Regression Rate and Combustion Efficiency of Composite Hybrid Rocket Grains Based on Modular Fuel Units 期刊论文  OAI收割 AEROSPACE, 2024, 卷号: 11, 期号: 4, 页码: 18 作者:  Pan JJ(潘俊杰);  Lin X(林鑫);  Wang ZZ(王泽众);  Wang RY(王若岩);  Wu K(吴坤)   |  收藏  |  浏览/下载：9/0  |  提交时间：2024/05/27 modular unit  modification  regression rate  combustion efficiency  hybrid rocket engine   Additively manufactured aluminium nested composite hybrid rocket fuel grains with breathable blades 期刊论文  OAI收割 VIRTUAL AND PHYSICAL PROTOTYPING, 2023, 卷号: 18, 期号: 1, 页码: e2235680 作者:  Qu DD(屈丹丹);  Lin X(林鑫);  Zhang K(张坤);  Li ZY(李志永);  Wang ZZ(王泽众)   |  收藏  |  浏览/下载：111/0  |  提交时间：2023/09/05 Hybrid rocket engine  additive manufacturing  three-dimensional printing  breathable blade  composite fuel grain  mechanical and combustion properties  porous structure  >   Combustion Characteristics of a Swirl-Radial-Injection Composite Fuel Grain with Applications in Hybrid Rockets 期刊论文  OAI收割 AEROSPACE, 2023, 卷号: 10, 期号: 9, 页码: 19 作者:  Wang, Ruoyan;  Lin, Xin;  Wang, Zezhong;  Wu, Kun;  Zhang, Zelin   |  收藏  |  浏览/下载：21/0  |  提交时间：2023/10/30 hybrid rocket engine  swirl-radial injection  regression rate  flame images  combustion efficiency   Charactering Catalytic Ignition and Combustion for the Ninety Percent Hydrogen Peroxide/Paraffin Based Hybrid Rocket Engine 期刊论文  OAI收割 JOURNAL OF PROPULSION AND POWER, 2023 作者:  Wang ZZ(王泽众);  Lin X(林鑫);  Wu K(吴坤);  Zhang ZL(张泽林);  Fang SH(方思晗)   |  收藏  |  浏览/下载：16/0  |  提交时间：2023/04/20 Hybrid Rocket Engines  Propellant  Thermocouples  Numerical Analysis  Catalysis  Absorption Spectroscopy  Combustion Products  decomposition efficiency  Paraffin Fuel  Ignition Systems   Flame Dynamics in the Combustion Chamber of Hybrid Rocket Using Multiangle Chemiluminescence 期刊论文  OAI收割 JOURNAL OF PROPULSION AND POWER, 2023 作者:  Luo JX(罗家枭);  Zhang ZL(张泽林);  Lin X(林鑫);  Wang ZZ(王泽众);  Wu K(吴坤)   |  收藏  |  浏览/下载：24/0  |  提交时间：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  OAI收割 ACTA ASTRONAUTICA, 2022, 卷号: 199, 页码: 174-182 作者:  Zhang, Zelin;  Lin, Xin;  Wang, Zezhong;  Wu, Kun;  Luo, Jiaxiao   |  收藏  |  浏览/下载：38/0  |  提交时间：2022/11/08 Hybrid rocket engine  Swirl injection  Novel composite fuel grain  Regression rate  Oxidizer-to-fuel ratio   Three-dimensional printed metal-nested composite fuel grains with superior mechanical and combustion properties 期刊论文  OAI收割 VIRTUAL AND PHYSICAL PROTOTYPING, 3, 2022, 卷号: 17, 页码: 437 作者:  Lin X(林鑫);  Qu DD(屈丹丹);  Chen XD(陈雪冬);  Wang ZZ(王泽众);  Luo JX(罗家枭)   |  收藏  |  浏览/下载：30/0  |  提交时间：2022/10/23 Hybrid rocket engine  additive manufacturing  metal-nested composite fuel grain  mechanical properties  combustion properties  optical emission spectroscopy   Determining the time-resolved mass flow rates of hybrid rocket fuels using laser absorption spectroscopy 期刊论文  OAI收割 ACTA ASTRONAUTICA, 2021, 卷号: 188, 页码: 110-120 作者:  Wang ZZ(王泽众);  Lin X(林鑫);  Li F(李飞);  Peng JL(彭锦龙);  Liu, Yan   |  收藏  |  浏览/下载：49/0  |  提交时间：2021/11/01 Hybrid rocket engine  Fuel mass flow rate  Tunable diode laser absorption spectroscopy  Temperature  Partial pressure