跪求。。翼型以及翼型風(fēng)洞實(shí)驗(yàn)數(shù)據(jù)

追風(fēng)信子

如題

ljhmiao

謝謝jsdjj900了，好東西

最終大戰(zhàn)

如題

qqshanquan

謝謝分享，需要用用

新角色

這些東西大部分都是公開(kāi)的，國(guó)內(nèi)哪來(lái)的什么機(jī)密文件，所謂的機(jī)密文件都是買(mǎi)國(guó)外設(shè)計(jì)，老外ctrl+v給你的。國(guó)內(nèi)有葉片的風(fēng)洞數(shù)據(jù)嗎

qiaoyinhu

謝謝分享！

laney

木有~有也不給~ [s:7]

lgzll

機(jī)密資料,下跪別人也不敢給你.

niho

我來(lái)貼一個(gè)吧, 沒(méi)這么玄乎, Riso的公開(kāi)資料, 放附件太大, 大家自己下吧~

http://www.risoe.dk/Risoe_dk/Hom ... rts/ris-r-1280.aspx

Wind Turbine Airfoil Catalogue
Franck Bertagnolio, Niels Sørensen, Jeppe Johansen and Peter Fuglsang

Risø National Laboratory, August 2001, 152 p., ISBN 87-550-2911-6
Risø-R-1280(EN) 2,7 Mb

Abstract

The aim of this work is two-sided. Firstly, experimental results obtained for numerous sets of airfoil measurements (mainly intended for wind turbine applications) are collected and compared with computational results from the 2D Navier-Stokes solver EllipSys2D, as well as results from the panel method code XFOIL. Secondly, we are interested in validating the code EllipSys2D and finding out for which airfoils it does not perform well compared to the experiments, as well as why, when it does so. The airfoils are classified according to the agreement between the numerical results and experimental data. A study correlating the available data and this classification is performed. It is found that transition modelling is to a large extent responsible for the poor quality of the computational results for most of the considered airfoils. The transition model mechanism that leads to these discrepancies is identified. Some advices are given for elaborating future airfoil design processes that would involve the numerical code EllipSys2D in particular, and transition modelling in general.

laney

還是樓上兄弟慷慨哦~
俺小心眼兒啦~
其實(shí)很多翼型都是公開(kāi)的
NACA.... [s:1]