Application of DES Method to the Numerical Study of Shock Oscillations on a Supercritical Airfoil

Tao Yang, H. Yong, Wei Zhi, L. Guangyuan
{"title":"Application of DES Method to the Numerical Study of Shock Oscillations on a Supercritical Airfoil","authors":"Tao Yang, H. Yong, Wei Zhi, L. Guangyuan","doi":"10.1109/ISDEA.2012.625","DOIUrl":null,"url":null,"abstract":"The periodical shock oscillations phenomenon induced by transonic shock/turbulence boundary layer interaction is a major cause of transonic buffet. Detached Eddy Simulation (DES) method is applied to study the self-sustained shock oscillations phenomenon of SC (2)-0714 supercritical airfoil in this paper. The periodic shock motion on the upper surface of the airfoil is predicted with the DES method in calculations. The effects of Reynolds number on the shrinkage-reduce frequency of the shock motion, mean shock position and coefficients of fluctuating pressures are also studied in the paper.","PeriodicalId":267532,"journal":{"name":"2012 Second International Conference on Intelligent System Design and Engineering Application","volume":null,"pages":null},"PeriodicalIF":0.0000,"publicationDate":"2012-04-03","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2012 Second International Conference on Intelligent System Design and Engineering Application","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ISDEA.2012.625","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0

Abstract

The periodical shock oscillations phenomenon induced by transonic shock/turbulence boundary layer interaction is a major cause of transonic buffet. Detached Eddy Simulation (DES) method is applied to study the self-sustained shock oscillations phenomenon of SC (2)-0714 supercritical airfoil in this paper. The periodic shock motion on the upper surface of the airfoil is predicted with the DES method in calculations. The effects of Reynolds number on the shrinkage-reduce frequency of the shock motion, mean shock position and coefficients of fluctuating pressures are also studied in the paper.
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
DES方法在超临界翼型激波振荡数值研究中的应用
跨声速激波与湍流边界层相互作用引起的周期性激波振荡现象是跨声速振动的主要原因。采用分离涡模拟(DES)方法研究了SC(2)-0714超临界翼型的自持续激波振荡现象。在计算中采用DES方法对翼型上表面的周期激波运动进行了预测。本文还研究了雷诺数对激波运动收缩-减小频率、平均激波位置和脉动压力系数的影响。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 去求助
来源期刊
自引率
0.00%
发文量
0
期刊最新文献
Application of DES Method to the Numerical Study of Shock Oscillations on a Supercritical Airfoil The Topological Detection Algorithm of Object Arrays in Noisy Context Based on Fuzzy Spatial Information Fusion and Prim Algorithm Robust Adaptive Fuzzy Tracking Control of Stochastic Neuron Systems A Framework for Agent-Based Collaborative Information Processing in Distributed Sensor Network Hydro Generation Scheduling Using Refined Genetic Algorithm
×
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