鼻锥整流罩和尖顶对超音速钝体流动的影响

IF 1.3 4区 工程技术 Q2 ENGINEERING, AEROSPACE
MD. G. Sarwar, Priyank Kumar, S. Das
{"title":"鼻锥整流罩和尖顶对超音速钝体流动的影响","authors":"MD. G. Sarwar, Priyank Kumar, S. Das","doi":"10.2514/1.a35757","DOIUrl":null,"url":null,"abstract":"Experiments and computations were performed at Mach number 2.0 for various nose cone fairing bodies with a sharp spike and conical spike of [Formula: see text] and with a sharp spike having a fixed tip location of different [Formula: see text] ratios. Attempts were made to alter the flowfield of various nose cone fairing bodies with the adoption of the spike. Qualitative and quantitative measurement studies indicate the changes that support the reduction of drag forces, not only on hemispherical blunt bodies but also on various nose cone fairings. This drag reduction with the configurations tested in this study indicates the importance of the region between the spike and the blunt-body face. The results presented here justify the quality and quantity of recirculating flow and its implication for drag reduction.","PeriodicalId":50048,"journal":{"name":"Journal of Spacecraft and Rockets","volume":"94 1","pages":""},"PeriodicalIF":1.3000,"publicationDate":"2023-11-20","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Influence of Nose Cone Fairing and Spike on Supersonic Blunt Body Flows\",\"authors\":\"MD. G. Sarwar, Priyank Kumar, S. Das\",\"doi\":\"10.2514/1.a35757\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Experiments and computations were performed at Mach number 2.0 for various nose cone fairing bodies with a sharp spike and conical spike of [Formula: see text] and with a sharp spike having a fixed tip location of different [Formula: see text] ratios. Attempts were made to alter the flowfield of various nose cone fairing bodies with the adoption of the spike. Qualitative and quantitative measurement studies indicate the changes that support the reduction of drag forces, not only on hemispherical blunt bodies but also on various nose cone fairings. This drag reduction with the configurations tested in this study indicates the importance of the region between the spike and the blunt-body face. The results presented here justify the quality and quantity of recirculating flow and its implication for drag reduction.\",\"PeriodicalId\":50048,\"journal\":{\"name\":\"Journal of Spacecraft and Rockets\",\"volume\":\"94 1\",\"pages\":\"\"},\"PeriodicalIF\":1.3000,\"publicationDate\":\"2023-11-20\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Journal of Spacecraft and Rockets\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://doi.org/10.2514/1.a35757\",\"RegionNum\":4,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q2\",\"JCRName\":\"ENGINEERING, AEROSPACE\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Journal of Spacecraft and Rockets","FirstCategoryId":"5","ListUrlMain":"https://doi.org/10.2514/1.a35757","RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
引用次数: 0

摘要

在马赫数为 2.0 时,对各种鼻锥整流罩体进行了实验和计算,这些鼻锥整流罩体带有[计算公式:见正文]的尖头和锥形尖头,以及具有不同[计算公式:见正文]比率的固定尖头位置的尖头。尝试通过采用尖头来改变各种鼻锥整流罩的流场。定性和定量测量研究表明,不仅半球形钝体,而且各种鼻锥整流罩上的变化都有助于减少阻力。本研究中测试的配置所产生的阻力减少表明了尖头和钝体表面之间区域的重要性。本文介绍的结果证明了再循环流的质量和数量及其对减少阻力的影响。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Influence of Nose Cone Fairing and Spike on Supersonic Blunt Body Flows
Experiments and computations were performed at Mach number 2.0 for various nose cone fairing bodies with a sharp spike and conical spike of [Formula: see text] and with a sharp spike having a fixed tip location of different [Formula: see text] ratios. Attempts were made to alter the flowfield of various nose cone fairing bodies with the adoption of the spike. Qualitative and quantitative measurement studies indicate the changes that support the reduction of drag forces, not only on hemispherical blunt bodies but also on various nose cone fairings. This drag reduction with the configurations tested in this study indicates the importance of the region between the spike and the blunt-body face. The results presented here justify the quality and quantity of recirculating flow and its implication for drag reduction.
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
Journal of Spacecraft and Rockets
Journal of Spacecraft and Rockets 工程技术-工程:宇航
CiteScore
3.60
自引率
18.80%
发文量
185
审稿时长
4.5 months
期刊介绍: This Journal, that started it all back in 1963, is devoted to the advancement of the science and technology of astronautics and aeronautics through the dissemination of original archival research papers disclosing new theoretical developments and/or experimental result. The topics include aeroacoustics, aerodynamics, combustion, fundamentals of propulsion, fluid mechanics and reacting flows, fundamental aspects of the aerospace environment, hydrodynamics, lasers and associated phenomena, plasmas, research instrumentation and facilities, structural mechanics and materials, optimization, and thermomechanics and thermochemistry. Papers also are sought which review in an intensive manner the results of recent research developments on any of the topics listed above.
×
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
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
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 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术官方微信