Developing a mathematical model of aircraft honeycomb sandwiches

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Abstract

A vibrational model of a three- layer honeycomb sandwich with partial skin peeling has been developed. The impact of peeling amount on the natural frequency of vibration and the amplitude-frequency characteristic has been analysed. Comparative analysis of design values and experimentally obtained results has been made.

About the authors

S. N. Tits

Samara State Aerospace University

Author for correspondence.
Email: intdep@ssau.ru
Russian Federation

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Copyright (c) 2015 VESTNIK of the Samara State Aerospace University

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