Güneş A.Şahin Ö.A.2020-03-262020-03-2620161897-2764https://dx.doi.org/10.5604/18972764.1229632https://hdl.handle.net/20.500.12395/34319Purpose: The purpose of this paper investigates to stiffness behavior of hybrid laminated composites with surface crack. Design/methodology/approach: Hybrid laminated composites has 18 layers and 90x25 mm size with two different layers line up. The low velocity impact test of hybrid laminated composites carried on 3 m/sec with a/t=0.4 and a/c=0.4 surface crack parameters. Findings: The results are presented as the change of force-time and force-displacement graphs. As a result of this study, effects of stacking sequence on hybrid composite plates were analysed. Research limitations/implications: The research of stiffness behavior or dynamic response of hybrid laminated composites can contribute to developing new composite materials. Practical implications: These hybrid laminated composites materials could be used for different aviation areas. Originality/value: This paper is based on studies from Selçuk University and all the experiments and results were conducted by me. © by International OCSCO World Press. All rights reserved. 2016.en10.5604/18972764.1229632info:eu-repo/semantics/openAccessLaminated compositeLow velocity impactSurface crackArticle8024952Q3