Email this article 
Developing a mathematical model of aircraft honeycomb sandwiches
- Authors: Tits S.N.1
-
Affiliations:
- Samara State Aerospace University
- Issue: Vol 7, No 1 (2008)
- Pages: 80-91
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/546
- DOI: https://doi.org/10.18287/2541-7533-2008-0-1(14)-80-91
- ID: 546
Cite item
Full Text
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
References
Supplementary files
