To Solution of the Optimization Problem for the Small Dimension Engine Core Turbine Wheel Space

A. E. Remizov; V. V. Vyatkov; E. S. Osokina; R. V. Kharchenko

doi:10.3103/S1068799819010240

To Solution of the Optimization Problem for the Small Dimension Engine Core Turbine Wheel Space

作者: Remizov A.E.¹, Vyatkov V.V.¹, Osokina E.S.¹, Kharchenko R.V.¹
隶属关系:
1. P.A. Soloviev Rybinsk State Aviation Technical University
期: 卷 62, 编号 1 (2019)
页面: 167-170
栏目: Aircraft and Rocket Engine Theory
URL: https://journals.rcsi.science/1068-7998/article/view/230890
DOI: https://doi.org/10.3103/S1068799819010240
ID: 230890

如何引用文章

全文:

开放存取

##reader.subscriptionAccessGranted##
受限制的访问

订阅存取

详细
作者简介
参考
补充文件
统计

详细

The paper considers the optimization problems in high-pressure turbine gas-dynamic design based on the ANSYS CFX software package. It is shown that the optimization procedure formation and predicted optimization results depend on the turbine dimension. The best results of the gas-dynamic optimization can be achieved, when turbines with aerodynamically long blades are designed.