A novel PHDAL-MCDNN framework for reliability assessment of turbine blades under combined high and low cycle fatigue
Fields of Study & Subjects
High Temperature Alloys and Creep
Bladed Disk Vibration Dynamics
Probabilistic and Robust Engineering Design
Publication details
- Journal / source
- Aerospace Science and Technology
- Publisher
- Elsevier BV
- Volume
- 177
- Pages
- 112352–112352
- Publication date
- 12 April 2026
- Language
- EN