Dynamic analysis of the composite laminated repaired perforated plates by using multi-patch IGA method |
| |
Authors: | Jamshid FAZILATI Vahid KHALAFI |
| |
Affiliation: | Aeronautical Science and Technology Department, Aerospace Research Institute, Tehran 14657-74111, Iran;Aerospace Engineering Department, Shahid Sattari Aeronautical University of Science and Technology, Tehran, Iran |
| |
Abstract: | The bonded repair techniques seem to be the most frequent procedures in the aviation maintenance. The achieved composite repaired perforated thin-walled plate is a complex geometry with high numerical analysis cost. The NURBS-based Isogeometric Analysis (IGA) proposes a sensible and affordable tool to carry out such geometry analysis. In this context, a well-known technique is to divide the original geometry assembly into number of simple neighbors connected geometries. In the present study the free vibration analysis of the perforated plates repaired on one side with an external bonded composite laminated patch is investigated. A multi-patch geometry modeling approach is implemented in line with the first order shear deformation theory of plates. In order to hold the geometry integrity and uniformity, all the degrees of freedom between adjacent geometry patches are completely tied through implementing a Nitsche method. To show the effectiveness and accuracy of the developed formulation, some representative results are extracted and compared with those from literature. The effects of geometrical as well as material parameters including boundary condition, cutout shape, and repair layup on the dynamic response of the repaired perforated plates are then investigated. |
| |
Keywords: | Composite laminate Perforated plate Bonded repair Isogeometric analysis (IGA) Multi-patch model |
本文献已被 万方数据 ScienceDirect 等数据库收录! |
|