Concepts of Gas Turbine Engine Improvement Through the Use of Choked-Flow Turbines


如何引用文章

全文:

开放存取 开放存取
受限制的访问 ##reader.subscriptionAccessGranted##
受限制的访问 订阅存取

详细

The new conceptual design of simple gas turbine engines for different purposes is presented. A choked-flow low-pressure turbine is used that allows reducing the number of stages and gas temperature in the relative motion ahead of blades. Application of such turbines with uncooled blades to reduce the cost of power-limited engines is considered.

作者简介

V. Bogdanov

Solov’ev Rybinsk State Aviation Technical University

编辑信件的主要联系方式.
Email: bogdanov-vasiliy@yandex.ru
俄罗斯联邦, ul. Pushkina 53, Rybinsk, 152934

补充文件

附件文件
动作
1. JATS XML

版权所有 © Allerton Press, Inc., 2018