- 收听数
- 0
- 性别
- 保密
- 听众数
- 23
- 最后登录
- 2024-2-19
- QQ
 - UID
- 2826
- 阅读权限
- 40
- 帖子
- 2223
- 精华
- 0
- 在线时间
- 2729 小时
- 注册时间
- 2013-1-27
- 科研币
- 26
- 速递币
- 22350
- 娱乐币
- 2910
- 文献值
- 903
- 资源值
- 10
- 贡献值
- 0
|
速递书局
| 封面: |
 |
| 题名: |
Advances in Simulation of Wing and Nacelle Stall: Results of the Closing Symposium of the DFG Research Unit FOR 1066, December 1–2, 2014, Braunschweig, Germany |
| 作者: |
Rolf Radespiel, Reinhard Niehuis, Norbert Kroll, Kathrin Behrends |
| 出版社: |
Springer |
| 出版日期: |
2015 |
| ISBN: |
9783319211268 |
| 附属页: |
齐全 |
| 书签: |
有 |
| 格式: |
清晰PDF |
| 内容简介: |
The book reports on advanced solutions to the problem of simulating wing and nacelle stall, as presented and discussed by internationally recognized researchers at the Closing Symposium of the DFG Research Unit FOR 1066. Reliable simulations of flow separation on airfoils, wings and powered engine nacelles at high Reynolds numbers represent great challenges in defining suitable mathematical models, computing numerically accurate solutions and providing comprehensive experimental data for the validation of numerical simulations. Additional problems arise from the need to consider airframe-engine interactions and inhomogeneous onset flow conditions, as real aircraft operate in atmospheric environments with often-large distortions. The findings of fundamental and applied research into these and other related issues are reported in detail in this book, which targets all readers, academics and professionals alike, interested in the development of advanced computational fluid dynamics modeling for the simulation of complex aircraft flows with flow separation. |
| 求助帖链接: |
http://www.expaper.cn/forum.php?mod=viewthread&tid=93792&extra=page%3D1 |
本帖子中包含更多资源
您需要 登录 才可以下载或查看，没有帐号？快速注册
-
总评分: 速递币 + 50
文献值 + 2
查看全部评分
|
发表于 2015-7-20 21:14:20
淘帖
收藏
顶
踩
