找回密碼
 To register

QQ登錄

只需一步,快速開始

掃一掃,訪問微社區(qū)

打印 上一主題 下一主題

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

[復(fù)制鏈接]
查看: 13534|回復(fù): 57
樓主
發(fā)表于 2025-3-21 16:35:57 | 只看該作者 |倒序瀏覽 |閱讀模式
書目名稱Drag Reduction by Shock and Boundary Layer Control
副標(biāo)題Results of the Proje
編輯Egon Stanewsky,Jean Délery,Paolo Matteis
視頻videohttp://file.papertrans.cn/283/282758/282758.mp4
概述Covers shock control uniquely.Sequel to NNFM 56
叢書名稱Notes on Numerical Fluid Mechanics and Multidisciplinary Design
圖書封面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
關(guān)鍵詞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

書目名稱Drag Reduction by Shock and Boundary Layer Control影響因子(影響力)




書目名稱Drag Reduction by Shock and Boundary Layer Control影響因子(影響力)學(xué)科排名




書目名稱Drag Reduction by Shock and Boundary Layer Control網(wǎng)絡(luò)公開度




書目名稱Drag Reduction by Shock and Boundary Layer Control網(wǎng)絡(luò)公開度學(xué)科排名




書目名稱Drag Reduction by Shock and Boundary Layer Control被引頻次




書目名稱Drag Reduction by Shock and Boundary Layer Control被引頻次學(xué)科排名




書目名稱Drag Reduction by Shock and Boundary Layer Control年度引用




書目名稱Drag Reduction by Shock and Boundary Layer Control年度引用學(xué)科排名




書目名稱Drag Reduction by Shock and Boundary Layer Control讀者反饋




書目名稱Drag Reduction by Shock and Boundary Layer Control讀者反饋學(xué)科排名




單選投票, 共有 0 人參與投票
 

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

您所在的用戶組沒有投票權(quán)限
沙發(fā)
發(fā)表于 2025-3-21 20:27:44 | 只看該作者
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.
板凳
發(fā)表于 2025-3-22 03:06:00 | 只看該作者
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.
地板
發(fā)表于 2025-3-22 06:58:34 | 只看該作者
5#
發(fā)表于 2025-3-22 10:04:27 | 只看該作者
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.
6#
發(fā)表于 2025-3-22 14:55:38 | 只看該作者
7#
發(fā)表于 2025-3-22 20:35:25 | 只看該作者
8#
發(fā)表于 2025-3-22 23:46:55 | 只看該作者
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.
9#
發(fā)表于 2025-3-23 03:21:40 | 只看該作者
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.
10#
發(fā)表于 2025-3-23 07:43:09 | 只看該作者
 關(guān)于派博傳思  派博傳思旗下網(wǎng)站  友情鏈接
派博傳思介紹 公司地理位置 論文服務(wù)流程 影響因子官網(wǎng) 吾愛論文網(wǎng) 大講堂 北京大學(xué) Oxford Uni. Harvard Uni.
發(fā)展歷史沿革 期刊點評 投稿經(jīng)驗總結(jié) SCIENCEGARD IMPACTFACTOR 派博系數(shù) 清華大學(xué) Yale Uni. Stanford Uni.
QQ|Archiver|手機版|小黑屋| 派博傳思國際 ( 京公網(wǎng)安備110108008328) GMT+8, 2026-1-30 02:26
Copyright © 2001-2015 派博傳思   京公網(wǎng)安備110108008328 版權(quán)所有 All rights reserved
快速回復(fù) 返回頂部 返回列表
河南省| 洞头县| 景东| 长沙县| 江川县| 马龙县| 汾西县| 沾化县| 东阳市| 金沙县| 锦屏县| 普兰店市| 开阳县| 米林县| 大余县| 凌云县| 周宁县| 乌审旗| 同仁县| 武宁县| 昌乐县| 定襄县| 肇源县| 黑山县| 晋城| 蒙自县| 龙门县| 冕宁县| 重庆市| 龙泉市| 冷水江市| 定日县| 呼图壁县| 泸溪县| 阳西县| 云安县| 历史| 巧家县| 包头市| 莱阳市| 博罗县|