| Download | - View final version: Stress and fracture mechanics analysis of the six stage compressor spacer of the J85-CAN-40 engine (PDF, 8.2 MiB)
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| DOI | Resolve DOI: https://doi.org/10.4224/40003867 |
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| Author | Search for: Beres, W.1 |
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| Affiliation | - National Research Council Canada. NRC Institute for Aerospace Research
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| Format | Text, Technical Report |
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| Physical description | 40 p. |
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| Abstract | Results of finite element based stress and fracture mechanics analyses carried out on the sixth stage compressor spacer of the J85-CAN-40 engine using three dimensional models are presented. It was established that bolt holes located at both, forward and aft, spacer flanges are the fracture critical locations. Stress intensity factors for cracks emanating from these bolt holes change only moderately with crack lengths. |
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| Publication date | 1997-03 |
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| Publisher | National Research Council Canada |
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| Series | |
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| Language | English |
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| Peer reviewed | No |
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| Export citation | Export as RIS |
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| Report a correction | Report a correction (opens in a new tab) |
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| Record identifier | f2c30478-90c9-4e17-98df-d8331cdc74f5 |
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| Record created | 2025-11-14 |
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| Record modified | 2025-11-14 |
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