Wall Heat Flux Measurements for a Kerosene-Fueled Supersonic Combustor

Cheng Di; Wang Jing; Lu Yang; Li Long; Yao Wei; Fan Xuejun

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Wall Heat Flux Measurements for a Kerosene-Fueled Supersonic Combustor

机译：煤油燃料超音速燃烧器的壁热通量测量

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摘要

Wall heat flux distributions under different configurations for a kerosene-fueled supersonic combustor were experimentally studied. The influences of combustion, global fuel equivalence ratio, mass flow rate, total temperature, and inlet Mach number on the wall heat flux of the kerosene-fueled supersonic combustor were systematically presented and analyzed for the first time. Methods to calibrate and validate the in-house-developed heat flux sensors are also presented. The revealed trends would be useful to guide the design of thermal management systems for kerosene-fueled scramjets.

机译：实验研究了煤油燃料超音速燃烧器在不同构型下的壁热通量分布。首次系统地分析和分析了燃烧，总燃料当量比，质量流量，总温度和进气马赫数对煤油燃料超音速燃烧器壁热通量的影响。还介绍了校准和验证内部开发的热通量传感器的方法。揭示的趋势将有助于指导煤油燃料超燃冲压发动机的热管理系统的设计。

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来源
《Journal of aerospace engineering》 |2019年第5期|04019080.1-04019080.11|共11页
作者
Cheng Di; Wang Jing; Lu Yang; Li Long; Yao Wei; Fan Xuejun;
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作者单位

China Acad Aerosp Aerodynam, Res & Dev Ctr, Beijing 100074, Peoples R China|Univ Connecticut, Dept Mech Engn, Storrs, CT 06269 USA;

Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China;

Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China;

Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China;

Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China|Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China;

Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China|Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China;

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正文语种 eng
中图分类
关键词
Heat flux measurement; Kerosene; Supersonic combustion; Scramjet; Heat flux sensor;

机译：热量磁通测量;煤油;超音速燃烧;斯普拉克喷射;热通量传感器;

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专利

1. Wall Heat Flux Measurements for a Kerosene-Fueled Supersonic Combustor [J] . Cheng Di, Wang Jing, Lu Yang, Journal of aerospace engineering . 2019,第5期

机译：煤油燃料超声波燃烧器的壁热通量测量
2. Application of conjugate gradient method for estimation of the wall heat flux of a supersonic combustor [J] . Liuwei Cheng, Fengquan Zhong, Hongbin Gu, International Journal of Heat and Mass Transfer . 2016,第May期

机译：共轭梯度法在超音速燃烧室壁热通量估算中的应用
3. Effects of Entry Conditions on Cracked Kerosene-Fueled Supersonic Combustor Performance [J] . Xuejun Fan, Gong Yu, Jianguo Li, Combustion Science and Technology . 2007,第10a12期

机译：进入条件对裂解煤油燃料超音速燃烧器性能的影响
4. Measurements of Wall Heat Flux and Temperature in a Supersonic Model Combustor [C] . Long Li, Xuejun Fan, Jing Wang AIAA/ASME/SAE/ASEE joint propulsion conference exhibit . 2012

机译：超音速模型燃烧器壁热通量和温度的测量
5. Thermal characterization and heat transfer study of a gasoline homogeneous charge compression ignition engine via measurements of instantaneous wall temperature and heat flux in the combustion chamber. [D] . Chang, Junseok. 2004

机译：通过测量燃烧室的瞬时壁温和热通量，对汽油均质充量压缩点火发动机进行热特性和传热研究。
6. Local data of heat flux wall temperature and the void phase along the boiling curve during vertical subcooled flow boiling of refrigerant Novec 649 at a copper wall [O] . Moritz Bruder, Ludwig Sembach, Veronika Krumova, 2018

机译：制冷剂Novec 649在铜壁上的垂直过冷流动沸腾过程中沿沸腾曲线的热通量壁温和空隙相的局部数据
7. Wall Heat Flux Measurements for a Kerosene-Fueled Supersonic Combustor [O] . Di Cheng, Jing Wang, Yang Lu, 2019

机译：煤油燃料超声波燃烧器的壁热通量测量
8. Benchmark Wall Heat Flux Data for a GO2/CH2 Single Element Combustor [R] . Marshall, W. M. , Pal, S. , Woodward, R. D. , 2005

机译：GO2 / CH2单元件燃烧器的基准壁热通量数据

Wall Heat Flux Measurements for a Kerosene-Fueled Supersonic Combustor

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