Examination of Honeycomb Core Compliance in Sandwich Structure
Dominik Nowakowski
Air Force Institute of TechnologyWarsaw, Poland
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, , , Sylwester Kłysz
- Air Force Institute of TechnologyWarsaw, Poland
- University of Warmia and Mazury in OlsztynOlsztyn, Poland
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e 15 lug 2020
INFORMAZIONI SU QUESTO ARTICOLO
Pubblicato online: 15 lug 2020
Pagine: 19 - 27
DOI: https://doi.org/10.2478/fas-2019-0003
Parole chiave
© 2019 Dominik Nowakowski et al., published by Sciendo
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.
The objective of the research presented in this paper was to determine the honeycomb core compliance of a sandwich structure of the horizontal stabilizer of the MiG-29 fighter jet in the static compression test. The study of the specimen was conducted based on the ASTM C365/C365M standard. The article presents the results of experimentally determined dependencies and strength parameters, i.e. the force-displacement dependence, the compressive modulus and the honeycomb core deformations.