Postbuckling analysis of pultruded composite bars and simple frames

 
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1997 (EN)

Postbuckling analysis of pultruded composite bars and simple frames (EN)

Raftoyiannis, IG (EN)
Kounadis, AN (EN)

A simplified but very reliable approach for the postbuckling analysis of pultruded composite bars and simple two-bar frames using the classical lamination theory is comprehensively presented. The overall postbuckling responses for symmetric I-structural shapes made from commercially available composite and homogeneous materials are thoroughly discussed. This leads to the optimum design of the structures under consideration. A simple stability criterion is also established for a direct determination of the critical loads. Two numerical examples are used to illustrate the simplicity and efficiency of the proposed procedure. (EN)

journalArticle (EN)

DELAMINATION (EN)
BEAMS (EN)
Engineering, Aerospace (EN)


AIAA Journal (EN)

English

1997 (EN)

10.2514/2.48 (EN)
12 (EN)
1887 (EN)
35 (EN)
ISI:A1997YJ07800012 (EN)
1881 (EN)
0001-1452 (EN)

AMER INST AERONAUT ASTRONAUT (EN)




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