G. I. Turchannikov

DOI Number: N/A

Conference number: IFASD-2015-200

The current work highlights the issues associated with the use of the unified computer model of an aircraft for multidisciplinary design, certification, and the structural monitoring during operation. The technology of using flight simulators for definition of structural loads of an aircraft had been developed and implemented. The database structure for storing and processing information had been formed.

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In Categories: 2. IFASD 2015, Poster presentations
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