电邮这篇文章 Weight optimization principles for turbine blade shroud platform
- 作者: Belousov A.I.1, Nazdrachev S.V.1
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隶属关系:
- Samara State Aerospace University
- 期: 卷 59, 编号 1 (2016)
- 页面: 51-57
- 栏目: Aircraft and Rocket Engine Design and Development
- URL: https://journals.rcsi.science/1068-7998/article/view/229557
- DOI: https://doi.org/10.3103/S1068799816010086
- ID: 229557
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详细
The paper describes the development of NK-family engine shrouded turbine blades. Weight optimization principles are formulated with account for strength and manufacturability limits.
作者简介
A. Belousov
Samara State Aerospace University
编辑信件的主要联系方式.
Email: aibelousov@mail.ru
俄罗斯联邦, shosse Moskovskoe 34, Samara, 443086
S. Nazdrachev
Samara State Aerospace University
Email: aibelousov@mail.ru
俄罗斯联邦, shosse Moskovskoe 34, Samara, 443086
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