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Flame Dynamics in the Combustion Chamber of Hybrid Rocket Using Multiangle Chemiluminescence

文献类型：期刊论文

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); Zhou GX(周功喜); Zhang SH(张森豪); Li F(李飞); Yu XL(余西龙); Wu, Jie3
刊名JOURNAL OF PROPULSION AND POWER
出版日期2023
ISSN号0748-4658
关键词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
DOI10.2514/1.B38955
英文摘要The flame dynamics in the combustion chamber of a hybrid rocket motor were visualized using novel chemiluminescence imaging. A multidirectional visualization system employing 3x1 endoscopes generated images based on methylidyne chemiluminescence (CH*), with one endoscope in the precombustion chamber and two in the postcombustion chamber. Images were collected with a high speed camera using a 1 ms exposure and a 1 kHz frame rate. Fuel grains having a helical or a conventional circular port structures were assessed, and combustion trials were conducted using a laboratory scale hybrid rocket motor with oxygen as the oxidizer at mass flow rates from 10.43 to 18.51 g/s: equivalent to combustion chamber pressures ranging from 0.7 to 1.24 MPa. Flame structures were observed during the ignition, combustion, and shutdown stages; and the helical grain generated a larger, more intense flame zone. A proper orthogonal decomposition analysis showed that the helical grains also produced a greater degree of turbulence and stronger oscillations. These results confirm that a helical structure increases the flow turbulence and convective heat transfer in the combustion chamber. These effects lead to higher regression rates and better mixing efficiency that may, in turn, provide greater combustion efficiency at optimized oxidizer/fuel ratios.
分类号二类
WOS研究方向Engineering, Aerospace
语种英语
WOS记录号WOS:000940164500001
资助机构National Natural Science Foundation of China [~92271117, 11802315, 11927803, 11872368, 12072355] ; Key Area Research and Development Program of Guangdong Province [~2021B0909060004] ; Youth Innovation Promotion Association of the Chinese Academy of Sciences [~2022018]
其他责任者Wang, ZZ (corresponding author), Univ Chinese Acad Sci, Inst Mech, Beijing 100049, Peoples R China. ; Wang, ZZ (corresponding author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China. ; Lin, X (corresponding author), Inst Mech, Beijing, Peoples R China.
源URL[http://dspace.imech.ac.cn/handle/311007/91836]  
专题力学研究所_高温气体动力学国家重点实验室
作者单位1.Inst Mech, Beijing, Peoples R China
2.Univ Chinese Acad Sci, Beijing 100049, Peoples R China
3.Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China
4.Sci & Technol Opt Radiat Lab, Beijing 100845, Peoples R China
5.Univ Chinese Acad Sci, Inst Mech, Beijing 100049, Peoples R China
6.Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China
7.North Univ China, Inst Mech, Taiyuan 030051, Peoples R China
8.North Univ China, Coll Mechatron Engn, Taiyuan 030051, Peoples R China
推荐引用方式
GB/T 7714		 Luo JX,Zhang ZL,Lin X,et al. Flame Dynamics in the Combustion Chamber of Hybrid Rocket Using Multiangle Chemiluminescence[J]. JOURNAL OF PROPULSION AND POWER,2023.
APA 罗家枭.,张泽林.,林鑫.,王泽众.,吴坤.,...&Wu, Jie.(2023).Flame Dynamics in the Combustion Chamber of Hybrid Rocket Using Multiangle Chemiluminescence.JOURNAL OF PROPULSION AND POWER.
MLA 罗家枭,et al."Flame Dynamics in the Combustion Chamber of Hybrid Rocket Using Multiangle Chemiluminescence".JOURNAL OF PROPULSION AND POWER (2023).

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来源：力学研究所

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