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...

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Bibliografische gegevens
Hoofdauteurs: A. A. Shanyavskiy, C. Bathia, A. D. Nikitin, T. Palin-Luk
Formaat: Artikel
Taal:Russisch
Gepubliceerd in: Moscow State Technical University of Civil Aviation 2016-11-01
Reeks:Научный вестник МГТУ ГА
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Online toegang:https://avia.mstuca.ru/jour/article/view/319
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