Influence of the Airfoil Leading Edge Thickness on Turbine Cascade Losses Due to the Incidence
- 作者: Mamaev B.I.1, Starodumov A.V.1, Poluboyarinova S.A.1
-
隶属关系:
- A. Lyul’ka Design Bureau
- 期: 卷 62, 编号 2 (2019)
- 页面: 274-280
- 栏目: Aircraft and Rocket Engine Design and Development
- URL: https://journals.rcsi.science/1068-7998/article/view/230951
- DOI: https://doi.org/10.3103/S1068799819020144
- ID: 230951
如何引用文章
详细
On the basis of experimental studies, it is established that the thickening of the airfoil leading edge at positive incidences increases the impingement resistance of the moderate convergence cascade, but it does not exert impact in the high convergence cascade, and practically does not affect losses in the cascade of any convergence at the negative incidences.
作者简介
B. Mamaev
A. Lyul’ka Design Bureau
Email: andrey.starodumov@okb.umpo.ru
俄罗斯联邦, ul. Kasatkina 13, Moscow, 129301
A. Starodumov
A. Lyul’ka Design Bureau
编辑信件的主要联系方式.
Email: andrey.starodumov@okb.umpo.ru
俄罗斯联邦, ul. Kasatkina 13, Moscow, 129301
S. Poluboyarinova
A. Lyul’ka Design Bureau
Email: andrey.starodumov@okb.umpo.ru
俄罗斯联邦, ul. Kasatkina 13, Moscow, 129301
补充文件
