Determination of the Crack Tip Position by Digital Image Correlation during Static and Cyclic Fracture Toughness Tests of Aluminum Alloys


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

Aluminum alloy V-1167RDTV specimens 1 mm thick with a central crack are used to determine the position of the tip of a mode I crack from a strain field distribution during cyclic loading in the course of fatigue crack growth rate tests and during static loading in determining the force characteristics of fracture toughness. When analyzing the displacement and strain distributions at the crack tip, we proposed a technique to measure the length of a statically growing crack to determine critical stress intensity factor Kc for a mode I crack in plane-stress state.

作者简介

V. Avtaev

All-Russia Institute of Aviation Materials

编辑信件的主要联系方式.
Email: darkee@mail.ru
俄罗斯联邦, Moscow, 105005

N. Yakovlev

All-Russia Institute of Aviation Materials

Email: darkee@mail.ru
俄罗斯联邦, Moscow, 105005

V. Erasov

All-Russia Institute of Aviation Materials

Email: darkee@mail.ru
俄罗斯联邦, Moscow, 105005

N. Podzhivotov

All-Russia Institute of Aviation Materials

Email: darkee@mail.ru
俄罗斯联邦, Moscow, 105005


版权所有 © Pleiades Publishing, Ltd., 2019
##common.cookie##