Crippling of Titanium Matrix Composite Stiffeners

Using established principles of laminate buckling theory and post buckling load redistribution, a theory is derived for crippling analysis of specially ortho tropic or very nearly specially orthotropic laminated composite stiffeners. Results from testing of SCS-6/Ti-15-3 titanium matrix composite (T...

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Veröffentlicht in:Journal of composite materials 1992-01, Vol.26 (7), p.991-1008
1. Verfasser: Fogarty, John H.
Format: Artikel
Sprache:eng
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Zusammenfassung:Using established principles of laminate buckling theory and post buckling load redistribution, a theory is derived for crippling analysis of specially ortho tropic or very nearly specially orthotropic laminated composite stiffeners. Results from testing of SCS-6/Ti-15-3 titanium matrix composite (TMC) stiffener segments are also presented and show good correlation with theoretical predictions. The testing program in cludes three different layups, three different geometries, and a repetition of two tests for each possible geometry/layup combination for a total of 18 tests. The results of the theory are presented in the form of easy-to-use design curves.
ISSN:0021-9983
1530-793X
DOI:10.1177/002199839202600703