Affiliation of Author(s):航空学院
Journal:INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES
Key Words:T-joint Composite structure Low velocity impact Delamination
Abstract:The purpose of this paper is to investigate the influence of fixed L-ribs on the damage behavior of integrated composite T-joints subject to low velocity impact. Experimental test is performed on a vertical drop-weight testing device with two different impact energies. Detailed inspection by visual and ultrasonic C-scan reveals that different impact energies result in different damage types and shapes. Experimental results show that without fixed L-ribs the impact caused an elliptical damage around the impact point at the impact energy of 4.45J/mm and a trumpet delamination at the impact energy of 8.90J/mm. In comparison, the impact only caused serious damage around the impact point without delamination at the impact energy of 8.90J/mm with fixed L-ribs. This experimental study has demonstrated that fixing the L-ribs is an effective way to prevent the delamination of the integrated composite T-joint subject to low velocity impact.
ISSN No.:2093-274X
Translation or Not:no
Date of Publication:2019-06-01
Co-author:Zhu, Rujian,mcj
Correspondence Author:xxw
Researcher
Education Level:南京航空学院
Degree:Doctoral Degree in Engineering
School/Department:College of Aerospace Engineering
Discipline:Engineering Mechanics. Solid Mechanics
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