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| 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 RY(王若岩); Lin X(林鑫) ; Wang ZZ(王泽众); Wu K(吴坤); Pan JJ(潘俊杰); Zhang ZL(张泽林); Luo JX(罗家枭); Li F(李飞); Yu XL(余西龙)
  Favorite | View/Download：15/0 | Submit date：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
JOURNAL OF SPACECRAFT AND ROCKETS, 2024, 页码: 9
Authors: Wang ZZ(王泽众); Lin X(林鑫); Pan JJ(潘俊杰); Luo JX(罗家枭); Wang RY(王若岩); Zhang ZL(张泽林); Yu XL(余西龙)
Favorite | View/Download：13/0 | Submit date：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
AEROSPACE, 2024, 卷号: 11, 期号: 4, 页码: 18
Authors: Pan JJ(潘俊杰); Lin X(林鑫); Wang ZZ(王泽众); Wang RY(王若岩); Wu K(吴坤); Liang, Jinhu; Yu XL(余西龙)
Favorite | View/Download：3/0 | Submit date：2024/05/27
modular unit modification regression rate combustion efficiency hybrid rocket engine |
| Multidimensional high-temperature field measurement method for flame based on near infrared radiation spectrum of water vapor 期刊论文
OPTICS AND LASERS IN ENGINEERING, 2024, 卷号: 174, 页码: 13
Authors: Zhou GX(周功喜); Wang, Wenjie; Li F(李飞); Lin X(林鑫); Meng DD(孟东东); Yu XL(余西龙)
Favorite | View/Download：138/0 | Submit date：2024/02/05
Multi-dimension High-temperature Self-Absorption Reconstruction algorithm |
| Combustion Characteristics of a Swirl-Radial-Injection Composite Fuel Grain with Applications in Hybrid Rockets 期刊论文
AEROSPACE, 2023, 卷号: 10, 期号: 9, 页码: 19
Authors: Wang RY(王若岩); Lin X(林鑫); Wang ZZ(王泽众); Wu K(吴坤); Zhang ZL(张泽林); Luo JX(罗家枭); Li F(李飞); Yu XL(余西龙)
Adobe PDF(8125Kb) | Favorite | View/Download：106/9 | Submit date：2023/10/30
hybrid rocket engine swirl-radial injection regression rate flame images combustion efficiency |
| Linear calibration-free wavelength modulation spectroscopy 期刊论文
MICROWAVE AND OPTICAL TECHNOLOGY LETTERS, 2023, 卷号: 65, 期号: 5, 页码: 1024-1030
Authors: Li RJ(李仁杰); Li F(李飞); Lin X(林鑫); Yu XL(余西龙)
Adobe PDF(2095Kb) | Favorite | View/Download：369/80 | Submit date：2021/11/01
calibration-free laser spectroscopy linear tunable diode laser absorption spectroscopy wavelength modulation spectroscopy |
| Research on flame temperature measurement method based on water vapor emission spectrum 期刊论文
MEASUREMENT SCIENCE AND TECHNOLOGY, 2023, 卷号: 34, 期号: 5, 页码: 10
Authors: Zhou GX(周功喜); Li F(李飞); Lin X(林鑫); Li RJ(李仁杰); Meng DD(孟东东); Yu XL(余西龙)
Adobe PDF(2336Kb) | Favorite | View/Download：188/9 | Submit date：2023/03/15
water vapor spectrum high temperature measurement self-absorption intensity ratio |
| 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：55/2 | 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 |
| Error Analysis of Integrated Absorbance for TDLAS in a Nonuniform Flow Field 期刊论文
APPLIED SCIENCES-BASEL, 2021, 卷号: 11, 期号: 22, 页码: 15
Authors: Li RJ(李仁杰); Li F(李飞); Lin X(林鑫); Yu XL(余西龙)
Adobe PDF(7410Kb) | Favorite | View/Download：258/47 | Submit date：2022/01/13
TDLAS integrated absorbance error analysis |
| 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：318/60 | Submit date：2021/11/01
Hybrid rocket engine Fuel mass flow rate Tunable diode laser absorption spectroscopy Temperature Partial pressure |
