找回密码
 To register

QQ登录

只需一步,快速开始

扫一扫,访问微社区

Titlebook: Drag Reduction by Shock and Boundary Layer Control; Results of the Proje Egon Stanewsky,Jean Délery,Paolo Matteis Conference proceedings 20

[复制链接]
查看: 13112|回复: 57
发表于 2025-3-21 16:35:57 | 显示全部楼层 |阅读模式
书目名称Drag Reduction by Shock and Boundary Layer Control
副标题Results of the Proje
编辑Egon Stanewsky,Jean Délery,Paolo Matteis
视频video
概述Covers shock control uniquely.Sequel to NNFM 56
丛书名称Notes on Numerical Fluid Mechanics and Multidisciplinary Design
图书封面Titlebook: Drag Reduction by Shock and Boundary Layer Control; Results of the Proje Egon Stanewsky,Jean Délery,Paolo Matteis Conference proceedings 20
描述The survival of the Aeronautical Industries of Europe in the highly competitive World Aviation Market is strongly dependent on such factors as time-to-market of a new or derivative aircraft and on its manufacturing costs but also on the achievement of a competitive technological advantage by which an increased market share can be gained. Recognizing this, cooperative research is continuously encouraged and co-financed by the European Union in order to strengthen the scientific and technological base of the Aeronautical Industries thus providing - among others - the technological edge needed for survival. Corresponding targets of research within Area 3, Technologies for Transport Means, and here in particular Area 3A, Aeronautics Technologies, of the Industrial and Materials Technologies Program ( Brite -EuRam III, 1994 -1998) have been identified to be aircraft efficiency, cost effectiveness and environmental impact. Concerning aircraft efficiency - relevant to the present research - a reduction in aircraft drag of 10%, a reduction in aircraft fuel consumption of 30%, and a reduction in airframe, engine and system weight of 20% are envisaged. Meeting these objectives has, of course
出版日期Conference proceedings 2002
关键词Fluid mechanics; aircraft engines; aircraft wings; boundary layers; flow control; modeling; shock waves; si
版次1
doihttps://doi.org/10.1007/978-3-540-45856-2
isbn_softcover978-3-642-07762-3
isbn_ebook978-3-540-45856-2Series ISSN 1612-2909 Series E-ISSN 1860-0824
issn_series 1612-2909
copyrightSpringer-Verlag Berlin Heidelberg 2002
The information of publication is updating

书目名称Drag Reduction by Shock and Boundary Layer Control影响因子(影响力)




书目名称Drag Reduction by Shock and Boundary Layer Control影响因子(影响力)学科排名




书目名称Drag Reduction by Shock and Boundary Layer Control网络公开度




书目名称Drag Reduction by Shock and Boundary Layer Control网络公开度学科排名




书目名称Drag Reduction by Shock and Boundary Layer Control被引频次




书目名称Drag Reduction by Shock and Boundary Layer Control被引频次学科排名




书目名称Drag Reduction by Shock and Boundary Layer Control年度引用




书目名称Drag Reduction by Shock and Boundary Layer Control年度引用学科排名




书目名称Drag Reduction by Shock and Boundary Layer Control读者反馈




书目名称Drag Reduction by Shock and Boundary Layer Control读者反馈学科排名




单选投票, 共有 0 人参与投票
 

0票 0%

Perfect with Aesthetics

 

0票 0%

Better Implies Difficulty

 

0票 0%

Good and Satisfactory

 

0票 0%

Adverse Performance

 

0票 0%

Disdainful Garbage

您所在的用户组没有投票权限
发表于 2025-3-21 20:27:44 | 显示全部楼层
Vassiliki Avgerinou,Stefanos G. Giakoumatosol on buffet onset..Two airfoils have been considered for the computations: the laminar DRA-2303 and the turbulent RAE-5225. Both airfoils were tested at DERA and hence experimental results were available allowing to make comparisons between the predicted numerical results and those obtained experimentally.
发表于 2025-3-22 03:06:00 | 显示全部楼层
Vassiliki Avgerinou,Stefanos G. Giakoumatosr damping of buffet. The 3D-unsteady code VIS25, developed at ONERA as an extension of the 2D VIS 15 code, has finally been used to study sweep effects on the flow with and without bump in the case of the ADIF sheared wing.
发表于 2025-3-22 06:58:34 | 显示全部楼层
发表于 2025-3-22 10:04:27 | 显示全部楼层
Hybrid and Active Control of Shock Wave — Turbulent Boundary Layer Interaction and Perforated Plate tension of the transpiration law has been derived which takes into account the effect of tangential stream along a porous plate..Numerical simulations have been extended to a 3-D analysis of the flow in a channel Here, it was found that 3-D effects are responsible for the discrepancy between experiment and 2-D calculations performed earlier.
发表于 2025-3-22 14:55:38 | 显示全部楼层
发表于 2025-3-22 20:35:25 | 显示全部楼层
发表于 2025-3-22 23:46:55 | 显示全部楼层
An Investigation of Active, Suction, Shock and Boundary Layer Control Techniquesfiguration of Active Suction does not reduce drag, but theoretical parametric studies have revealed a potential control system, which could be examined by a simple modification to the existing system. Hybrid Suction is shown to be in-effective at reducing drag.
发表于 2025-3-23 03:21:40 | 显示全部楼层
Introduction to the Individual Contributions of the work performed by the various members of EUROSHOCK II, written by these members. The contributions, Chapters 11 through 24, are assembled in the order of the four tasks which comprise the research project. The sequence of the individual contributions and the main contents of the research performed are briefly outlined below.
发表于 2025-3-23 07:43:09 | 显示全部楼层
 关于派博传思  派博传思旗下网站  友情链接
派博传思介绍 公司地理位置 论文服务流程 影响因子官网 SITEMAP 大讲堂 北京大学 Oxford Uni. Harvard Uni.
发展历史沿革 期刊点评 投稿经验总结 SCIENCEGARD IMPACTFACTOR 派博系数 清华大学 Yale Uni. Stanford Uni.
|Archiver|手机版|小黑屋| 派博传思国际 ( 京公网安备110108008328) GMT+8, 2025-5-14 10:54
Copyright © 2001-2015 派博传思   京公网安备110108008328 版权所有 All rights reserved
快速回复 返回顶部 返回列表