Abstract
The composite materials have a gained a tremendous usage in the areas of the aerospace, aeronautical and marine engineering areas. Due to such heavy usage of composites, many researchers are working on the topic of improving materials properties of the composites and tailoring their properties for a specific application. In the process of improving the composite materials, the researchers have identified hybridization as one of the decent methods for achieving better and tailored properties for the composite materials. In this paper, the effect of the stacking sequence arrangement on the mechanical and thermal properties of the hybrid laminates has been investigated. In this paper, two types of hybrid stacking arrangements namely sandwich and interlaced hybrid sequences has been investigated. Two different hybrid laminates namely kevlar49/S-glass laminas and IM7-carbon/boron lamina shave been developed and analyzed to know the generalized effectiveness of the hybrid stacking sequence. The modeling and analysis of the problem were performed using the MATLAB software. The properties of the individual lamina were found using finite element analysis implemented in ANSYS software.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
