Statistics: Ultrasonic inspection technique for composite doubler/aluminum skin bond integrity for aircraft

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This article is part of the collection entitled: Office of Scientific & Technical Information Technical Reports and was provided by UNT Libraries Government Documents Department to Digital Library, a digital repository hosted by the UNT Libraries. It has been viewed 44 times , with 7 in the last month . More information about this article can be viewed below.

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Year January February March April May June July August September October November December Total
2018 1 2 0 1 0 1 1 5 3 12 8 2 36
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2016 0 0 0 0 0 1 0 0 0 2 0 0 3

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