Developing an efficient FEM structural simulation of a fan blade off test in a turbofan jet engine
This work develops a methodology for full engine FEA simulation of the fan blade off containment test for a jet engine using LS-Dyna. The fan blade off containment test is a safety requirement involving the intentional release of a fan blade when the engine is running at full power. The released bla...
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| Format: | Others |
| Language: | en |
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University of Saskatchewan
2007
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| Online Access: | http://library.usask.ca/theses/available/etd-10292007-111221/ |