Fatigue crack growth from bolt holes of the 5th stage compressor discs of the J85-CAN-40 engines.
Fatigue crack growth from bolt holes of the 5th stage compressor discs of the J85-CAN-40 engines.
| Author | Search for: 1; Search for: 2 |
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| Affiliation |
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| Format | Text, Article |
| Conference | ICAS 2002 - 08-10 Sep 2002, Toronto |
| Subject | life prediction; gas turbine engine; fracture mechanics |
| Access condition |
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| Peer reviewed | Yes |
| NRC number | SMPL-2001-0179 |
| NPARC number | 8931378 |
| Export citation | Export as RIS |
| Report a correction | Report a correction (opens in a new tab) |
| Record identifier | 010f15b0-0148-451e-ba7d-461d1c4fe47a |
| Record created | 2009-04-23 |
| Record modified | 2020-04-17 |
- Date modified: