An analogy of RVE-based numerical model and experimental study of Charpy impact on thin carbon/aramid hybrid composites for micro/mini-Belly landing UAV fuselage.

Autor:	Zachariah, Sojan Andrews1,2, Dayananda, Pai K.1, Padmaraj N. H.1, Shenoy B., Satish1 satish.shenoy@manipal.edu
Zdroj:	Cogent Engineering. 2024, Vol. 11 Issue 1, p1-13. 13p.
Databáze:	Academic Search Ultimate
Externí odkaz:	Zobrazit plný text záznamu