碳氢燃料蓄热冷却工作状态图

IF 5.4 2区 工程技术 Q1 ENGINEERING, AEROSPACE Propulsion and Power Research Pub Date : 2023-06-01 DOI:10.1016/j.jppr.2023.05.002
Chen Zhang , Hui Gao , Jiajun Zhao , Guice Yao , Dongsheng Wen
{"title":"碳氢燃料蓄热冷却工作状态图","authors":"Chen Zhang ,&nbsp;Hui Gao ,&nbsp;Jiajun Zhao ,&nbsp;Guice Yao ,&nbsp;Dongsheng Wen","doi":"10.1016/j.jppr.2023.05.002","DOIUrl":null,"url":null,"abstract":"<div><p>Regenerative cooling by endothermic hydrocarbon fuel (EHF) is one of the most promising techniques for thermal management of supersonic or hypersonic aircraft. How to maintain the fuel working in proper states is an important issue to maximize the cooling potential of EHT. This work proposes a novel working state map, including risking zone (RZ), thermal cracking zone (TCZ), supercritical zone (SupZ) and subcritical zone (SubZ), to differentiate possible working states of an EHF during regenerative cooling. Using <em>n</em>-decane flowing in a circular tube as an example, the boundaries of four zones are determined by numerical simulation covering different heat fluxes (0.2–4.0 MW<strong>·</strong>m<sup>−2</sup>) and mass flow rates (0.5–10.5 g<strong>·</strong>s<sup>−1</sup>) under two operating pressures (3.45 and 5.00 MPa). Empirical correlations for three boundary lines are obtained and the maximum cooling capacity is identified, as well as the identification of the pressure effect. The revelation of such new perspective of regenerative cooling is of great implication to the design and optimization of cooling system for future thermal management.</p></div>","PeriodicalId":51341,"journal":{"name":"Propulsion and Power Research","volume":"12 2","pages":"Pages 199-211"},"PeriodicalIF":5.4000,"publicationDate":"2023-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Working state map of hydrocarbon fuels for regenerative cooling\",\"authors\":\"Chen Zhang ,&nbsp;Hui Gao ,&nbsp;Jiajun Zhao ,&nbsp;Guice Yao ,&nbsp;Dongsheng Wen\",\"doi\":\"10.1016/j.jppr.2023.05.002\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><p>Regenerative cooling by endothermic hydrocarbon fuel (EHF) is one of the most promising techniques for thermal management of supersonic or hypersonic aircraft. How to maintain the fuel working in proper states is an important issue to maximize the cooling potential of EHT. This work proposes a novel working state map, including risking zone (RZ), thermal cracking zone (TCZ), supercritical zone (SupZ) and subcritical zone (SubZ), to differentiate possible working states of an EHF during regenerative cooling. Using <em>n</em>-decane flowing in a circular tube as an example, the boundaries of four zones are determined by numerical simulation covering different heat fluxes (0.2–4.0 MW<strong>·</strong>m<sup>−2</sup>) and mass flow rates (0.5–10.5 g<strong>·</strong>s<sup>−1</sup>) under two operating pressures (3.45 and 5.00 MPa). Empirical correlations for three boundary lines are obtained and the maximum cooling capacity is identified, as well as the identification of the pressure effect. The revelation of such new perspective of regenerative cooling is of great implication to the design and optimization of cooling system for future thermal management.</p></div>\",\"PeriodicalId\":51341,\"journal\":{\"name\":\"Propulsion and Power Research\",\"volume\":\"12 2\",\"pages\":\"Pages 199-211\"},\"PeriodicalIF\":5.4000,\"publicationDate\":\"2023-06-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Propulsion and Power Research\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S2212540X23000330\",\"RegionNum\":2,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q1\",\"JCRName\":\"ENGINEERING, AEROSPACE\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Propulsion and Power Research","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S2212540X23000330","RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
引用次数: 0

摘要

利用吸热碳氢燃料(EHF)进行再生冷却是超声速或高超声速飞机热管理中最有前途的技术之一。如何保持燃料在适当的状态下工作是最大化EHT冷却潜力的一个重要问题。本文提出了一种新的工作状态图,包括危险区(RZ)、热裂解区(TCZ)、超临界区(SupZ)和亚临界区(SubZ),以区分再生冷却过程中EHF可能的工作状态。以正癸烷在圆管内流动为例,在3.45和5.00 MPa两种工作压力下,通过数值模拟确定了不同热流密度(0.2 ~ 4.0 MW·m−2)和质量流量(0.5 ~ 10.5 g·s−1)的四个区域边界。得到了三条边界线的经验相关性,并确定了最大制冷量,以及压力效应的识别。这种蓄热式冷却新视角的揭示,对未来热管理冷却系统的设计与优化具有重要意义。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
Working state map of hydrocarbon fuels for regenerative cooling

Regenerative cooling by endothermic hydrocarbon fuel (EHF) is one of the most promising techniques for thermal management of supersonic or hypersonic aircraft. How to maintain the fuel working in proper states is an important issue to maximize the cooling potential of EHT. This work proposes a novel working state map, including risking zone (RZ), thermal cracking zone (TCZ), supercritical zone (SupZ) and subcritical zone (SubZ), to differentiate possible working states of an EHF during regenerative cooling. Using n-decane flowing in a circular tube as an example, the boundaries of four zones are determined by numerical simulation covering different heat fluxes (0.2–4.0 MW·m−2) and mass flow rates (0.5–10.5 g·s−1) under two operating pressures (3.45 and 5.00 MPa). Empirical correlations for three boundary lines are obtained and the maximum cooling capacity is identified, as well as the identification of the pressure effect. The revelation of such new perspective of regenerative cooling is of great implication to the design and optimization of cooling system for future thermal management.

求助全文
通过发布文献求助,成功后即可免费获取论文全文。 去求助
来源期刊
CiteScore
7.50
自引率
5.70%
发文量
30
期刊介绍: Propulsion and Power Research is a peer reviewed scientific journal in English established in 2012. The Journals publishes high quality original research articles and general reviews in fundamental research aspects of aeronautics/astronautics propulsion and power engineering, including, but not limited to, system, fluid mechanics, heat transfer, combustion, vibration and acoustics, solid mechanics and dynamics, control and so on. The journal serves as a platform for academic exchange by experts, scholars and researchers in these fields.
期刊最新文献
Auto-updating model-based control for thrust variation mitigation and acceleration performance enhancement of gas turbine aero-engines Experimental study of corner separation and unsteady characteristics in linear compressor cascades with and without sweeping jet actuator Solitary, periodic, kink wave solutions of a perturbed high-order nonlinear Schrödinger equation via bifurcation theory Structural design of aeroengine radiators: State of the art and perspectives Entropy optimization on Casson nanofluid flow with radiation and Arrhenius activation energy over different geometries: A numerical and statistical approach
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 联系我们:info@booksci.cn
Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。
Copyright © 2023 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1