The computational method of vibration-dynamic condition of aeronautical engineering objects in extraordinary situations

Аuthors

Tishkov V. V.^*, Firsanov V. V.^**

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: tishkovvv@mai.ru
**e-mail: k906@mai.ru

Abstract

The computational method of vibration-dynamic condition of aeronautical engineering objects in extraordinary situations is considered. The regression model built based on integration of data obtained from an experiment with similar samples is cited.

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