Development of fatigue cracking in aircraft engine compressor disks of titanium alloy Ti-6A1-3Mo-2Cr

Fatigue and Fracture of Engineering Materials and Structures

Volumn 21, Issue 3, 1998, Pages 297-313

  Shaniavski, A A ^a   Losey, A I ^a   Banov, M D ^a  

^a State Civil Aviation Research Institute   (Russian Federation)

Author keywords

Aero engine disks; Failure in service; Hold times; Quantitative fractography; Ti 6A1 3Mo 2Cr titanium alloy; Vibrational loading

Indexed keywords

EID: 0012977132     PISSN: 8756758X     EISSN: None     Source Type: Journal    
DOI: 10.1046/j.1460-2695.1998.00021.x     Document Type: Article

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