Analysis of stress state in a root-airfoil transition zone of hollow wide chord fan blades


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

In this paper, under consideration is the complex approach to analyzing the operation of a simulator for the hollow blade made from the VT6 titanium alloy. The stress state parameters in the hollow-monolithic part transition zone of the cantilevered simulator at bending under the distributed load are determined.

作者简介

V. Berdin

Ufa State Aviation Technical University

编辑信件的主要联系方式.
Email: berdinvk@mail.ru
俄罗斯联邦, ul. Karla Marksa 12, Ufa, 450000

A. Smyslov

Ufa State Aviation Technical University

Email: berdinvk@mail.ru
俄罗斯联邦, ul. Karla Marksa 12, Ufa, 450000

N. Berdin

Ufa State Aviation Technical University

Email: berdinvk@mail.ru
俄罗斯联邦, ul. Karla Marksa 12, Ufa, 450000

V. Luk’yanov

Ufa State Aviation Technical University

Email: berdinvk@mail.ru
俄罗斯联邦, ul. Karla Marksa 12, Ufa, 450000


版权所有 © Allerton Press, Inc., 2016
##common.cookie##