Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
1634842 | Procedia Materials Science | 2014 | 5 Pages |
Abstract
The general block diagram of crack growth modeling and periodicity of aircraft elements controlling was worked out. The major factors determining the size of calculation inaccuracy under calculations of the crack growth duration and the inspections intervals was marked and estimated with the help of the diagram.
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