FATIGUE CRACKING MECHANISMS OF TITANIUM ALLOY VT3-1 IN VERY-HIGH-CYCLE-FATIGUE REGIME
Investigations and tests of specimens of VT3-1 titanium alloy were done in Very-High-Cycle-Fatigue regime. Specimens were manufactured from compressor disks of D30-KU engine, and tests under frequency 20 kHz performed on the special test-bed in laboratory of Paris University «ITMA». Crack originatio...
Guardat en:
| Autors principals: | , , , |
|---|---|
| Format: | Artigo |
| Idioma: | Russo |
| Publicat: |
Moscow State Technical University of Civil Aviation
2016-11-01
|
| Col·lecció: | Научный вестник МГТУ ГА |
| Matèries: | |
| Accés en línia: | https://avia.mstuca.ru/jour/article/view/319 |
| Etiquetes: |
Sense etiquetes, Sigues el primer a etiquetar aquest registre!
|