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Health Monitoring and Crack Detection System Development for Turbine Engine Rotating Components

The hot section components of jet engines undergo severe environmental operating conditions that generate combined thermo-mechanical loads, which impair their structural durability and performance. Minimizing the impact of these loads and inventing a crack detection technology to monitor the health of these components is among the key objectives of the National Aeronautics and Space Administration (NASA) Aviation Safety Program (AVSP)

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