Improved method for determining the stress relaxation at the crack tip


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详细

A technique is suggested to determine the stress relaxation at the crack tip during tests of a specimen of a new type at a constant crack opening fixed by a stay bolt. The shape and geometry of the specimen make it possible to set the load and to determine the crack closure force after long-term exposure using the force transducer of a tensile-testing machine. The stress relaxation at the crack tip is determined in a V95pchT2 alloy specimen at elevated temperatures.

作者简介

A. Grinevich

All-Russia Institute of Aviation Materials VIAM

编辑信件的主要联系方式.
Email: viam660@yandex.ru
俄罗斯联邦, ul. Radio 17, Moscow, 105005

V. Erasov

All-Russia Institute of Aviation Materials VIAM

Email: viam660@yandex.ru
俄罗斯联邦, ul. Radio 17, Moscow, 105005

V. Avtaev

All-Russia Institute of Aviation Materials VIAM

Email: viam660@yandex.ru
俄罗斯联邦, ul. Radio 17, Moscow, 105005


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