Analysis of Twisting Stiffness for a Multifiber Composite Layer

Author:

Bert C. W.1,Chang S.2

Affiliation:

1. School of Aerospace, Mechanical and Nuclear Engineering, University of Oklahoma, Norman, Okla.

2. Department of Aerospace Engineering, Mechanical Engineering and Engineering Mechanics, University of Alabama, University, Ala.

Abstract

The twisting stiffness of a rectangular cross section consisting of a single row of solid circular cross-section fibers embedded in a matrix is analyzed. The problem is formulated as a Dirichlet torsion problem of a multielement region and solved by the boundary-point least-squares method. Numerical results for a single-fiber square cross section compare favorably with previous relaxation-method results. New numerical results for three and five-fiber composites suggest that the torsional rigidity of a multifiber composite can be approximated from the torsional rigidities of single and three-fiber models.

Publisher

ASME International

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Many names of the Trefftz method;Engineering Analysis with Boundary Elements;2018-11

2. Elastic torsion of bars possessing regular polygon in cross-section using BCM;Computers & Structures;2005-12

3. Analysis of cord-rubber composite laminates under combined tension and torsion loading;Composites Part B: Engineering;1997-01

4. TORSIONAL STRESS ANALYSIS OF CORD-RUBBER COMPOSITE LAMINATES;Mechanics of Composite Materials and Structures;1995-06

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