Analysis of the natural composite material layers influence on the cantilever’s structural performance

In this study, with their high strength-to-weight ratio, adaptability, and lack of corrosion, composite materials are widely used in aircraft construction can be considered an acceptable metal substitute by all parties involved. Static load tests have been performed under identical conditions stresses, but the layer sequence was changed. The Ansys workbench ACP-pre is utilized to analyze data. Various deformations were found as a result this. There values 14.265 0.1335 for smallest z-direction deformation overall strain 3 examples. Boundary confirmed 1,500 N resultant force static condition. simulation results analyzed Four employed different order investigated these Sisal, Pineapple, Jute, Kenaf. numerical undertaken using structure 16.1 Version tool. Geometry has modeled meshed workbench. model verified convergence test. As output, total von Mises stresses explained accordingly. Numerical stated that maximum due applied at Z-axis. value 1.254 mm minimum 2.5 mm. Furthermore, entire body calculated. shown 1.1 mPa. Eventually, main aim achieved employing accordingly