2 articles published in Asrel Aerospace Research Letters with the keyword "Finite Element method": Numerical and Analytical Free Vibration Analysis of Composite Plate with Auxetic Core Layer and Functionally Graded Surface Layers; NUMERICAL SIMULATION OF LOW VELOCITY IMPACT BEHAVIOR APPLIED ON E/GLASS EPOXY LAMINATES
Kerim Gökhan Aktaş, MEHMET ALİ GÜVENÇ
Asrel Aerospace Research Letters, 2024, Vol 3, Issue 2, Page 158-174
In this study, the free vibration behavior of a sandwich plate with a re-entrant auxetic core layer placed between two functionally graded (FG) composite surface layers are analyzed. Both analytical and numerical methods are employed under various boundary conditions to investigate the free...
Tolunay DAĞ, Nur YILDIRIM, Yusuf Kepir, Mesut UYANER
Asrel Aerospace Research Letters, 2022, Vol 1, Issue 1, Page 1-10
In order to gain weight in aerospace vehicles, the tendency to materials with high specific strength has increased. As a result, composite materials quickly took its place in aviation industry and have replaced metals at most points. Studies on impact tests on these composites have gained...
FG plateAuxetic coreNavier methodSi3N4-Ni matrixE-Cam/EpoksiDüşük Hızlı DarbeNümerik AnalizSonlu Eleman YöntemiDarbe DavranışıE-Glass/EpoxyLow Velocity ImpactNumerical AnalysisImpact Behavior
