Damage tolerance of adhesively bonded pultruded GFRP double-strap joints

نویسندگان

چکیده

Compared with mechanical fastening, adhesive bonding offers numerous advantages in the joining of pultruded glass fiber reinforced polymer (GFRP) sections. However, one critical issue associated bonded joints is assessment their behavior considering bondline defects. This paper presents results an experimental investigation damage tolerance adhesively GFRP Double-strap specimens and without defects were prepared tested tension until failure. The location (five different locations bond length width directions), size (10%, 20%, 30% total area both shape (triangular, rectangular, square, circular, elliptical), number (between 1 8) within considered as variable parameters. reports discusses observed failure modes, load–displacement curves, joint capacities, effects Interface debonding was regions neighboring defects, delamination other areas. All exhibited a linear elastic response sudden brittle failure, regardless presence capacity reduction up to 33% could be significant if located at edges area. Defects shapes resulted similar reductions (21%). Furthermore, found more sensitive irregularly shaped (e.g., triangular) reducing effective mitigating than defect was.

برای دانلود باید عضویت طلایی داشته باشید

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

A Probabilistic Method to Predict the Strength of Adhesively Bonded Joints of Gfrp

Experimental and numerical investigations were carried out on adhesively bonded full-scale double lap joints from pultruded GFRP profiles with relatively thick adhesive layers, needed in infrastructure applications to compensate for tolerances. The influence of different geometrical parameters on the joint strength was investigated, namely the thickness of the adhesive layer (from 5 to 35 mm), ...

متن کامل

Computational Models of Adhesively Bonded Joints

Simulations using the Finite Element Method (FEM) play an increasingly important role in the design process of joints and fasteners in the aerospace industry. In order to utilize the potential of such adhesive bonding, there is an increasing need for effective and accurate computational methods. The geometry and the nature of an adhesive joint are, however, not so simple to describe effectively...

متن کامل

Propagation of ultrasonic Lamb waves in adhesively bonded lap joints

This paper considers the bonded joint as a multilayer structure that is analysed using the Transfer Matrix method. In this particular case three layers (two adherents and the adhesive) are considered. The study of this propagation problem may be developed from matrix formulations which describe elastic waves in layered media. This technique combines the theory of the dynamics of the continuum w...

متن کامل

Fatigue life and backface strain predictions in adhesively bonded joints

Fatigue life and backface strain predictions in adhesively bonded joints. A. Graner Solana, A.D. Crocombe* and I.A. Ashcroft a Faculty of Engineering and Physical Sciences (J5), University of Surrey, Guildford, Surrey GU2 7XH, UK. b Wolfson School of Mechanical and Manufacturing Engineering, Loughborough University, Leicestershire LE11 3TU, UK * Corresponding author. Tel: +44 1483 689194 Fax: +...

متن کامل

Analytical model of asymmetrical Mixed-Mode Bending test of adhesively bonded GFRP joint

This paper presents new analytical model of asymmetric mixed-mode bending (MMB) specimen of adhesively bonded pultruded GFRP joints. An easily applicable relationship for the calculation of the strain energy release rate of the asymmetric MMB specimens is proposed based on the beam theory. The model is capable to analyze stacking sequence as well as various crack propagation paths. In the paper...

متن کامل

ذخیره در منابع من


  با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید

ژورنال

عنوان ژورنال: Composite Structures

سال: 2021

ISSN: ['0263-8223', '1879-1085']

DOI: https://doi.org/10.1016/j.compstruct.2021.113625