A systems engineering design of a retirement for cause life management process for life-limited F110-GE-400 engine parts
çExtreme temperatures and high component rotational speeds within a gas turbine engine and design constraints limit engineers' ability to design all engine components to last for the expected service life of the engine. Under the United States Navy's current life management philosophy whe...
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| Format: | Dissertation |
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/41669 http://scholar.lib.vt.edu/theses/available/etd-03172010-020231/ |