Experimental investigation for temperature and emissivity by flame emission spectrum in a cavity of rocket based combined cycle combustor chamber-Reference-Cited by-同舟云学术

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Experimental investigation for temperature and emissivity by flame emission spectrum in a cavity of rocket based combined cycle combustor chamber

Published:2024-09 Issue: Volume:39 Page:114-122
ISSN:2214-9147
Container-title:Defence Technology
language:en
Short-container-title:Defence Technology

Author:

Cai Weiguang,Zheng Shu,Wang Yan,Liu Bing,Zhu Shaohua,Zhao Li,Lu Qiang

Funder

National Natural Science Foundation of China

Natural Science Foundation of Jiangsu Province

Fundamental Research Funds for the Central Universities

Publisher

Elsevier BV

Reference33 articles.

1. Optimal trajectory and heat load analysis of different shape lifting reentry vehicles for medium range application;StuI;Defence Technology,2015

2. Numerical studies on four-engine rocket exhaust plume impinging on flame deflectors with afterburning;Zhou;Defence Technology,2021

3. Thermal response modeling and analysis of hydrocarbon fuel transient flow and heat transfer at supercritical pressure;Wu;Int J Therm Sci,2023

4. Experimental study on ejector-to-ramjet mode transition in a divergent kerosene-fueled RBCC combustor with low total temperature inflow;Shi;Aero Sci Technol,2020

5. On the measurement of flame temperature and emissivity based on multispectral imaging technique;Zheng;Measurement,2022

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Measurement of slagging thickness on the heating surfaces of a 330 MW subcritical boiler based on mid-infrared imaging technology;Measurement;2025-02

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