发布求助
文献互助 智能选刊 最新文献

A Shock Fitting Technique For Hypersonic Flows Using Hexahedral Meshes

25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference Pub Date : 2023-05-27 DOI:10.2514/6.2023-3020
Karan H. Baliga, Ravindra Krishnamurthy, M. Spel, Samuel E. James, Vijay Sudharshanam
{"title":"A Shock Fitting Technique For Hypersonic Flows Using Hexahedral Meshes","authors":"Karan H. Baliga, Ravindra Krishnamurthy, M. Spel, Samuel E. James, Vijay Sudharshanam","doi":"10.2514/6.2023-3020","DOIUrl":null,"url":null,"abstract":"","PeriodicalId":280984,"journal":{"name":"25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference","volume":"63 6 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2023-05-27","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.2514/6.2023-3020","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0
分享
查看原文 本刊更多论文
基于六面体网格的高超声速激波拟合技术
本文章由计算机程序翻译，如有差异，请以英文原文为准。
求助全文
约1分钟内获得全文 求助全文
来源期刊
25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
自引率
0.00%
发文量
0
×
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
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