A Laminated Plate Model of an Adhesive-Bonded Taper-Taper Joint Under Tension-Reference-Cited by-同舟云学术

A Laminated Plate Model of an Adhesive-Bonded Taper-Taper Joint Under Tension

Published:1997-10-01 Issue:4 Volume:119 Page:408-414
ISSN:0094-4289
Container-title:Journal of Engineering Materials and Technology
language:en
Short-container-title:

Author:

Helms Jack E.¹,Yang Chihdar²,Pang Su-Seng²

Affiliation:

1. Albemarle Corporation, 451 Florida Street, Baton Rouge, LA 70801

2. Department of Mechanical Engineering, Louisiana State University, Baton Rouge, LA 70803

Abstract

An analytical model of the strain and stress distributions in a taper-taper adhesive-bonded joint between two composite flat plates has been developed using first-order laminated plate theory. A correction for transverse shear deformation effects was included. The model was derived under the assumption of plane strain in the adherends and consists of eighteen first-order, linear, coupled ordinary differential equations with variable coefficients. The model was solved numerically using the Linear Shooting Method. Finite element models were also developed to verify the results of the analytical model using the COSMOS/M commercial software package.

Publisher

ASME International

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science

Link

http://asmedigitalcollection.asme.org/materialstechnology/article-pdf/119/4/408/5494317/408_1.pdf

Reference22 articles.

1. COSMOS/M Finite Element System User Guide, Version 1.65A, 1992, Structural Research And Analysis Corporation.

2. Erdogan F. , and RatwaniM., 1971, “Stress Distribution in Bonded Joints,” Journal of Composite Materials, Vol. 5, pp. 378–393.

3. Goland, M., and Reissner, E., 1944, “The Stresses in Cemented Joints,” ASME JOURNAL OF APPLIED MECHANICS, pp. A-17-A-27.

4. Hart-Smith, L. J., 1973a, “Adhesive-Bonded Single-Lap Joints,” Douglas Aircraft Co., NASA Contract Report CR-112236.

5. Hart-Smith, L. J., 1973b, “Adhesive-Bonded Double-Lap Joints,” Douglas Aircraft Co., NASA Contract Report CR-112235.

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