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Fatigue assessment of data acquisition system under random vibration load for fixed wing aircraft

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This paper targets the reliability of Data Acquisition System through Fatigue assessment under Random Vibration conditions. The fixed wing aircraft generate the random vibrations during the entire sortie and are imposed on the avionics systems installed on the platform. | Fatigue assessment of data acquisition system under random vibration load for fixed wing aircraft

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Fatigue assessment of data acquisition system under random vibration load for fixed wing aircraft

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