A New Machine Learning Based Approach to NASA's Propulsion Engine Diagnostic Benchmark Problem
abstract: Gas turbine engine for aircraft propulsion represents one of the most physics-complex and safety-critical systems in the world. Its failure diagnostic is challenging due to the complexity of the model system, difficulty involved in practical testing and the infeasibility of creating homoge...
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| Format: | Dissertation |
| Language: | English |
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2015
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| Online Access: | http://hdl.handle.net/2286/R.I.29831 |