• 文献检索
  • 文档翻译
  • 深度研究
  • 学术资讯
  • Suppr Zotero 插件Zotero 插件
  • 邀请有礼
  • 套餐&价格
  • 历史记录
应用&插件
Suppr Zotero 插件Zotero 插件浏览器插件Mac 客户端Windows 客户端微信小程序
定价
高级版会员购买积分包购买API积分包
服务
文献检索文档翻译深度研究API 文档MCP 服务
关于我们
关于 Suppr公司介绍联系我们用户协议隐私条款
关注我们

Suppr 超能文献

核心技术专利:CN118964589B侵权必究
粤ICP备2023148730 号-1Suppr @ 2026

文献检索

告别复杂PubMed语法,用中文像聊天一样搜索,搜遍4000万医学文献。AI智能推荐,让科研检索更轻松。

立即免费搜索

文件翻译

保留排版,准确专业,支持PDF/Word/PPT等文件格式,支持 12+语言互译。

免费翻译文档

深度研究

AI帮你快速写综述,25分钟生成高质量综述,智能提取关键信息,辅助科研写作。

立即免费体验

高超音速流中带有多排圆盘刺的再入头锥的热保护用侧向单射流的影响:计算研究。

Influence of lateral single jets for thermal protection of reentry nose cone with multi-row disk spike at hypersonic flow: computational study.

机构信息

Geely Automotive Institute, Hangzhou Vocational & Technical College, Hangzhou, 310018, China.

Department of Civil Engineering, College of Engineering, Cihan University-Erbil, Erbīl, Iraq.

出版信息

Sci Rep. 2023 Apr 21;13(1):6549. doi: 10.1038/s41598-023-33739-2.

DOI:10.1038/s41598-023-33739-2
PMID:37085555
原文链接:https://pmc.ncbi.nlm.nih.gov/articles/PMC10121723/
Abstract

The main challenge for the advancement of current high-speed automotives is aerodynamic heating. In this study, the application of lateral jet for thermal protection of the high-speed automotives is extensively studied. The simulation of the lateral coolant jet is done via Computational fluid dynamic at high-velocity condition. Finding optimum jet configuration for reduction of the aerodynamic heating is the main goal of this research. Two different coolant jets (Helium and Carbon dioxide) are investigated as coolant jet and flow study and fuel penetration mechanism are fully presented. In addition, the thermal load on the main body of nose cone is compared for different configurations. Our results specify that the injection of lateral jet near the tip of spike is effective for thermal protection of main body via deflection of bow shock. Also, Carbon dioxide jet with lower diffusivity is more effective for the protection of forebody with multi-row disk from sever aerodynamic heating.

摘要

当前高速汽车发展的主要挑战是空气动力学加热。在这项研究中,广泛研究了侧向射流在高速汽车热保护中的应用。通过计算流体动力学在高速条件下对侧向冷却射流进行模拟。本研究的主要目标是找到最佳的射流配置以减少空气动力学加热。研究了两种不同的冷却剂射流(氦气和二氧化碳)作为冷却剂射流,并对流动研究和燃料渗透机制进行了全面介绍。此外,还比较了不同构型下对头部锥体主体的热负荷。我们的研究结果表明,在尖刺尖端附近喷射侧向射流通过偏导弓形激波对主体进行有效的热保护。此外,具有较低扩散性的二氧化碳射流更有效地保护多排圆盘的头部免受严重的空气动力学加热。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/0c05/10121723/d8700ea6c7e0/41598_2023_33739_Fig9_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/0c05/10121723/45f44939b41c/41598_2023_33739_Fig1_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/0c05/10121723/fb086a4fe505/41598_2023_33739_Fig2_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/0c05/10121723/e342e142343d/41598_2023_33739_Fig3_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/0c05/10121723/94e0fb781cac/41598_2023_33739_Fig4_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/0c05/10121723/bfceacf29469/41598_2023_33739_Fig5_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/0c05/10121723/84ff0a645b94/41598_2023_33739_Fig6_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/0c05/10121723/04f51524c9c8/41598_2023_33739_Fig7_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/0c05/10121723/ba0ac7c860eb/41598_2023_33739_Fig8_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/0c05/10121723/d8700ea6c7e0/41598_2023_33739_Fig9_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/0c05/10121723/45f44939b41c/41598_2023_33739_Fig1_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/0c05/10121723/fb086a4fe505/41598_2023_33739_Fig2_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/0c05/10121723/e342e142343d/41598_2023_33739_Fig3_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/0c05/10121723/94e0fb781cac/41598_2023_33739_Fig4_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/0c05/10121723/bfceacf29469/41598_2023_33739_Fig5_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/0c05/10121723/84ff0a645b94/41598_2023_33739_Fig6_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/0c05/10121723/04f51524c9c8/41598_2023_33739_Fig7_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/0c05/10121723/ba0ac7c860eb/41598_2023_33739_Fig8_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/0c05/10121723/d8700ea6c7e0/41598_2023_33739_Fig9_HTML.jpg

相似文献

1
Influence of lateral single jets for thermal protection of reentry nose cone with multi-row disk spike at hypersonic flow: computational study.高超音速流中带有多排圆盘刺的再入头锥的热保护用侧向单射流的影响:计算研究。
Sci Rep. 2023 Apr 21;13(1):6549. doi: 10.1038/s41598-023-33739-2.
2
Numerical investigation of compressible flow around nose cone with Multi-row disk and multi coolant jets.多排圆盘和多冷却剂射流的头部锥形可压缩流的数值研究。
Sci Rep. 2023 Jan 16;13(1):787. doi: 10.1038/s41598-023-28127-9.
3
Influence of coolant multi-jets on heat reduction of nose cone with blunt spike at hypersonic flow.冷却剂多股射流对高超声速流中带钝头尖钉头锥热减少的影响。
Sci Rep. 2022 Sep 16;12(1):15615. doi: 10.1038/s41598-022-20046-5.
4
Numerical study of lateral coolant jet on heat reduction over nose cone with double-aerodome at hypersonic flow.高超音速流中侧向冷却剂射流对双穹顶头锥热降影响的数值研究
Sci Rep. 2022 Nov 27;12(1):20391. doi: 10.1038/s41598-022-22061-y.
5
Influence of extruded injector nozzle on fuel mixing and mass diffusion of multi fuel jets in the supersonic cross flow: computational study.挤压式喷油嘴对超音速横流中多燃料射流燃料混合和质量扩散的影响:计算研究
Sci Rep. 2023 Jul 26;13(1):12095. doi: 10.1038/s41598-023-39306-z.
6
Application of a Gas-Kinetic BGK Scheme in Thermal Protection System Analysis for Hypersonic Vehicles.气体动力学BGK格式在高超声速飞行器热防护系统分析中的应用。
Entropy (Basel). 2022 Sep 21;24(10):1325. doi: 10.3390/e24101325.
7
Penetration Characteristics of Air, Carbon Dioxide and Helium Transverse Sonic Jets in Mach 5 Cross Flow.马赫数5横流中空气、二氧化碳和氦气横向声速射流的穿透特性
Sensors (Basel). 2014 Dec 8;14(12):23462-23489. doi: 10.3390/s141223462.
8
Large-Eddy Simulation on the Aerodynamic and Thermal Characteristics in a Micropipe of the Hypersonic Engine Precooler.高超声速发动机预冷器微管道内气动和热特性的大涡模拟
Micromachines (Basel). 2022 Apr 17;13(4):637. doi: 10.3390/mi13040637.
9
Jet flow in steadily swimming adult squid.成年鱿鱼稳定游动时的射流
J Exp Biol. 2005 Mar;208(Pt 6):1125-46. doi: 10.1242/jeb.01507.
10
Effect of Kerosene Dual-Jet Spacing on the Mixing and Combustion Characteristics of a Scramjet Combustor.煤油双射流间距对超燃冲压发动机燃烧室混合与燃烧特性的影响
ACS Omega. 2024 Jul 24;9(31):33482-33493. doi: 10.1021/acsomega.4c00622. eCollection 2024 Aug 6.

引用本文的文献

1
Usage of serpentine injector for hydrogen mixing at combustion chamber of scramjet engine via a computational study.通过计算研究,探讨蛇形喷射器在超燃冲压发动机燃烧室中用于氢气混合的应用。
Sci Rep. 2025 Apr 16;15(1):13089. doi: 10.1038/s41598-025-98077-x.
2
Prediction of the transient coolant jet released from the nose cone at supersonic flow via machine learning.通过机器学习预测在超音速流中从鼻锥释放的瞬态冷却剂射流。
Sci Rep. 2025 Jan 28;15(1):3516. doi: 10.1038/s41598-025-87926-4.
3
Usage of double injector for efficient mixing of the fuel behind the ramp injector at supersonic combustion chamber.

本文引用的文献

1
Numerical investigation of compressible flow around nose cone with Multi-row disk and multi coolant jets.多排圆盘和多冷却剂射流的头部锥形可压缩流的数值研究。
Sci Rep. 2023 Jan 16;13(1):787. doi: 10.1038/s41598-023-28127-9.
2
Splitting of droplet with different sizes inside a symmetric T-junction microchannel using an electric field.在对称 T 型微通道中使用电场分裂不同尺寸的液滴。
Sci Rep. 2022 Feb 25;12(1):3226. doi: 10.1038/s41598-022-07130-6.
3
Numerical modeling of surface reaction kinetics in electrokinetically actuated microfluidic devices.
在超音速燃烧室中使用双喷射器以实现斜板喷射器后方燃料的高效混合。
Sci Rep. 2025 Jan 7;15(1):1151. doi: 10.1038/s41598-025-85215-8.
4
Investigation of unswept ramp system with lobe shape nozzle for fuel mixing of hydrogen jet at a scramjet engine.超燃冲压发动机中用于氢气射流燃料混合的带叶形喷嘴的未清扫斜板系统研究。
Sci Rep. 2024 Oct 9;14(1):23555. doi: 10.1038/s41598-024-75075-z.
5
Computational modeling of the rectangular non-aligned multi-injector for efficient fuel mixing in a supersonic combustion chamber.用于超声速燃烧室高效燃料混合的矩形非对齐多喷嘴的计算建模。
Sci Rep. 2024 Jul 10;14(1):15959. doi: 10.1038/s41598-024-66309-1.
6
Influence of the non-equal aligned nozzles for fuel injection inside the supersonic combustion chamber.超声速燃烧室内非等距排列喷油嘴对燃油喷射的影响。
Sci Rep. 2024 Jun 4;14(1):12812. doi: 10.1038/s41598-024-63544-4.
7
Using shock generator for the fuel mixing of the extruded single 4-lobe nozzle at supersonic combustion chamber.使用激波发生器在超音速燃烧室中对挤压式单四叶喷嘴进行燃料混合。
Sci Rep. 2024 Mar 17;14(1):6405. doi: 10.1038/s41598-024-57103-0.
8
Application of multi-extruded fuel injectors for mixing enhancement of hydrogen gas at scramjet engine: computational study.用于超燃冲压发动机氢气混合增强的多喷孔燃油喷射器应用:计算研究
Sci Rep. 2023 Nov 1;13(1):18839. doi: 10.1038/s41598-023-46217-6.
9
Fuel mixing enhancement of transverse coaxial air and fuel jet by upstream shock wave on in scramjet engines: numerical study.超燃冲压发动机中上游激波对横向同轴空气和燃料射流的燃料混合增强作用:数值研究
Sci Rep. 2023 Oct 28;13(1):18501. doi: 10.1038/s41598-023-45810-z.
10
Usage of extruded diamond multi-injectors for improvement of fuel mixing inside the supersonic combustion chamber.使用挤压式金刚石多喷嘴改善超音速燃烧室内的燃料混合。
Sci Rep. 2023 Sep 16;13(1):15393. doi: 10.1038/s41598-023-42487-2.
电动驱动微流控装置中表面反应动力学的数值模拟
Anal Chim Acta. 2014 Aug 1;838:64-75. doi: 10.1016/j.aca.2014.05.023. Epub 2014 May 21.