Ensemble of secondary cracks near the fatigue fracture surface of a titanium alloy VT23M specimen
- Авторлар: Lavrov A.1, Erasov V.1, Nochovnaya N.1, Kotova E.1
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Мекемелер:
- FGUP All-Russia Institute of Aviation Materials VIAM
- Шығарылым: Том 2017, № 4 (2017)
- Беттер: 330-333
- Бөлім: Diagnostics and Mechanical Test Techniques
- URL: https://journals.rcsi.science/0036-0295/article/view/171455
- DOI: https://doi.org/10.1134/S0036029517040127
- ID: 171455
Дәйексөз келтіру
Аннотация
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.
Авторлар туралы
A. Lavrov
FGUP All-Russia Institute of Aviation Materials VIAM
Хат алмасуға жауапты Автор.
Email: admin@viam.ru
Ресей, ul. Radio 17, Moscow, 105005
V. Erasov
FGUP All-Russia Institute of Aviation Materials VIAM
Email: admin@viam.ru
Ресей, ul. Radio 17, Moscow, 105005
N. Nochovnaya
FGUP All-Russia Institute of Aviation Materials VIAM
Email: admin@viam.ru
Ресей, ul. Radio 17, Moscow, 105005
E. Kotova
FGUP All-Russia Institute of Aviation Materials VIAM
Email: admin@viam.ru
Ресей, ul. Radio 17, Moscow, 105005
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