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- W2005333516 abstract "An analytical study was conducted using fracture mechanics principles to model turbine airfoil cracking. It was found that crack initiation can be related to calculated residual strains in the airfoil coating and that coating properties are an important consideration in determining crack location and orientation. The coating crack subsequently propagates into base material according to basic fracture mechanics laws. A comparison with engine tested blade experience is made. It is concluded that the presented model provides a rational method for design life prediction but its general application requires definition of new types of material property information." @default.
- W2005333516 created "2016-06-24" @default.
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- W2005333516 date "1975-03-02" @default.
- W2005333516 modified "2023-09-25" @default.
- W2005333516 title "A Fracture Mechanics Approach to Turbine Airfoil Design" @default.
- W2005333516 doi "https://doi.org/10.1115/75-gt-79" @default.
- W2005333516 hasPublicationYear "1975" @default.
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