Embedded delamination growth in composite panels under compressive load-Reference-Cited by-同舟云学术

Embedded delamination growth in composite panels under compressive load

Published:2001-04 Issue:3 Volume:32 Page:209-218
ISSN:1359-8368
Container-title:Composites Part B: Engineering
language:en
Short-container-title:Composites Part B: Engineering

Author:

Riccio A.,Scaramuzzino F.,Perugini P.

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites

Reference24 articles.

1. Approximate analysis of postbuckled through-the-width delaminations;Whitcomb;Composite Technol Rev,1982

2. Parametric analytical study of instability-related delamination growth;Whitcomb;Composite Sci Technol,1986

3. One delamination modelling of failure in laminated plates by delamination buckling;Chai;Int J Solids Struct,1981

4. Ashizawa M. Fast interlaminar fracture of a compressively loaded composite containing a defect. In: Proceedings of the Fifth DOD/NASA Conference on Fibrous Composites in Structural Design, NASA Ames Research Centre, 1981, p. 1-269–92.

5. Ramkumar RL. Fatigue degradation in compressively loaded composite laminates, NASA CR-165681, 1981.

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