journal article·2006-11

On the use of quasi-dynamic modeling for composite material structures: Analysis of adhesively bonded joints with midplane asymmetry and transverse shear deformation

Joshua Radice, Jack Vinson

Composites Science and Technology· Volume 66· Issue 14
Publisher page

Abstract

Abstract Adhesively bonded joints offer an attractive alternative to bolted/riveted approaches to joining load bearing elements because of potential weight savings and enhanced joint strength efficiency. However, modeling of these joints including substrate asymmetry, anisotropy, thickness variation, transverse shear deformation, hygrothermal growth, and complicated models for the adhesive layer can prove to be very unwieldy. This paper presents a solution methodology to model adhesively bonded joints which is capable of handling these important effects. The differential equations of motion are modified to include fictional damping type terms. Using a modified form of the thin structural displacements including temporal variation, the quasi-dynamic governing equations for thin plates are developed. The plate relationships are simplified to yield the quasi-dynamic beam/rod relationships. An assortment of boundary and initial conditions in terms of displacements are included for completeness and to facilitate implementation. To acquire quantitative solutions, the quasi-dynamic relationships are recast into the form of finite difference equations. A form suitable for the solution of a wide range of practical problems is presented. For completeness, the boundary and initial conditions are also recast into finite difference form. Justification of the choice to include the fictional damping terms and the discrete solution methodology is presented. The discrete governing equations are verified using the classical cantilevered beam case. Deviations from the classical solution resulting from the inclusion of transverse shear deformation and solution convergence are discussed. Once the quasi-dynamic solution methodology is validated, the single lap shear joint is modeled. Finally, a parametric study is performed to determine the influence of asymmetric adherend stiffness property variations on the peel and shear stresses in the adhesive layer. It is observed that decreases in adherend lumped shear stiffness results in reductions in the adhesive layer stress peaks. It is also observed that asymmetrically constructed adherends are of potential benefit to the reduction of adhesive peel stresses.
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Research context

OpenAlex topics: Mechanical Behavior of Composites · Composite Structure Analysis and Optimization · Structural Analysis and Optimization

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

References (17)

Show source-provided references
1. Adhesive bonding of polymer composites10.1002/pen.760291904 ↗
2. Kuno JK. Structural adhesives and bonding. In: Structural adhesives and bonding conference, 1979.
3. Kutcha D, Hofer KE, Jr., Feasibility of joining advanced composite flight vehicles, 1969.
4. Matthews · 1987
5. Volkersen O. Luftfahrt Forshungen, 1938.
6. The stresses in cemented joints
7. Analysis of adhesive bonded joints, square-end, and spew fillet-high order theory approach10.1061/(ASCE)0733-9399(1999)125:11(1298) ↗
8. Mortensen F, Thomsen OT. Analysis of adhesive bonded joints: a unified approach, 2002.10.1016/S0266-3538(02)00030-1 ↗
9. Vinson JR, Xiao Shengkuan. On the use of midplane asymmetric laminates for adhesively bonded joints in composite structures. In: 3rd Canadian Conference on Composite Materials, 2001.
10. Coupling effects in adhesive bonded joints10.1016/S0263-8223(02)00002-8 ↗
11. Use of asymmetric sandwich construction to minimize bending stresses
12. Circular cylindrical sandwich shells with mid-plane asymmetry subjected to axially symmetric loads
13. Vinson JR, Chen Z. Non-circular cylindrical shells of mid-plane asymmetric construction subjected to an internal pressure. In: Presented at the ASME IMECE, Nashville, November, 1999.
14. Vinson JR, Preissner E. Theory for midplane asymmetric sandwich cylindrical shells, J Sandwich Struct Mater, 2003.10.1177/1099636203005003002 ↗
15. Vinson JR, Sierakowski RL. The behavior of structures composed of composite materials.
16. Shear property measurements of adhesives in composite material bonded joints
17. Evaluation and adjustments for ASTM D 5656 standard test method for thick metal lap-shear joints for determination of the stress–strain behavior of adhesives in shear by tension loading10.1520/JTE12389J ↗