Effect of Parameters of Adhesive Application by Intaglio Printing on Honeycomb Core Bonding Strength

Author:

Kondratiev AndriiORCID,Melnikov SergiyORCID,Nabokina TetyanaORCID,Tsaritsynskyi AntonORCID

Publisher

Springer International Publishing

Reference22 articles.

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2. Fomin, O., Lovska, A., Kulbovskyi, I., et al.: Determining the dynamic loading on a semi-wagon when fixing it with a viscous coupling to a ferry deck. Eastern-European J. Enterp. Technol. (2019). https://doi.org/10.15587/1729-4061.2019.160456

3. Nunes, J.P., Silva, J.F.: Sandwiched composites in aerospace engineering. In: Rana, S., Fangueiro, R. (eds.) Advanced Composite Materials for Aerospace Engineering, pp. 129–174. Woodhead Publishing, Duxford (2016). https://doi.org/10.1016/B978-0-08-100037-3.00005-5

4. Slyvyns’kyy, V., Gajdachuk, V., Kirichenko, V., Kondratiev, A.: Basic parameters’ optimization concept for composite nose fairings of launchers. In: Proceedings of the 62nd International Astronautical Congress (IAC 2011), vol. 7, pp. 5701–5710 (2011)

5. Slyvynskyi, V.I., Sanin, A.F., Kharchenko, M.E., Kondratyev, A.V.: Thermally and dimensionally stable structures of carbon-carbon laminated composites for space applications. In: Proceedings of the International Astronautical Congress (IAC), vol. 8, pp. 5739–5751 (2014)

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