Turan, Kadir2024-04-242024-04-2420140021-99831530-793Xhttps://doi.org/10.1177/0021998313508801https://hdl.handle.net/11468/18043In this study, buckling behavior of adhesively patch repaired composite plates was investigated experimentally and numerically. Unidirectional carbon/epoxy composite plates with circular cutout were repaired with an adhesively bonded patch. Critical buckling loads of composite plates were researched without cutout, circular cutout, single patch-repaired, and double patch-repaired conditions. In addition to circular hole dimensions, patch length and adhesive thickness were used as geometrical parameters. Numerical study was performed in ANSYS finite element software three dimensionally. As a result, the critical buckling loads of single and double patch-repaired composite plates were increased from 96 and 263 ratios higher than circular-cutout composite plates. The percentile errors between experimental and numerical studies were determined from 2 to 11.5.eninfo:eu-repo/semantics/closedAccessComposite PlateBucklingAdhesively Patch RepairFinite Element MethodArticle482632533261WOS:0003440674000062-s2.0-8490888653210.1177/0021998313508801Q1Q2