Ensemble of secondary cracks near the fatigue fracture surface of a titanium alloy VT23M specimen
- 作者: Lavrov A.1, Erasov V.1, Nochovnaya N.1, Kotova E.1
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隶属关系:
- FGUP All-Russia Institute of Aviation Materials VIAM
- 期: 卷 2017, 编号 4 (2017)
- 页面: 330-333
- 栏目: Diagnostics and Mechanical Test Techniques
- URL: https://journals.rcsi.science/0036-0295/article/view/171455
- DOI: https://doi.org/10.1134/S0036029517040127
- ID: 171455
如何引用文章
详细
The secondary fragment cracks in a specimen made of a high-strength VT23M titanium alloy in the plane parallel to the specimen plane are studied with a scanning laser microscope. Two types of the secondary cracks are detected. Relations between the characteristics of an ensemble of secondary cracks and the cyclic loading parameters are obtained.
作者简介
A. Lavrov
FGUP All-Russia Institute of Aviation Materials VIAM
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Email: admin@viam.ru
俄罗斯联邦, ul. Radio 17, Moscow, 105005
V. Erasov
FGUP All-Russia Institute of Aviation Materials VIAM
Email: admin@viam.ru
俄罗斯联邦, ul. Radio 17, Moscow, 105005
N. Nochovnaya
FGUP All-Russia Institute of Aviation Materials VIAM
Email: admin@viam.ru
俄罗斯联邦, ul. Radio 17, Moscow, 105005
E. Kotova
FGUP All-Russia Institute of Aviation Materials VIAM
Email: admin@viam.ru
俄罗斯联邦, ul. Radio 17, Moscow, 105005
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