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...

وصف كامل

التفاصيل البيبلوغرافية
الحاوية / القاعدة:Научный вестник МГТУ ГА
المؤلفون الرئيسيون: A. A. Shanyavskiy, C. Bathia, A. D. Nikitin, T. Palin-Luk
التنسيق: مقال
اللغة:الروسية
منشور في: Moscow State Technical University of Civil Aviation 2016-11-01
الموضوعات:
الوصول للمادة أونلاين:https://avia.mstuca.ru/jour/article/view/319