Numerical/experimental evaluation of buckling behaviour and residual tensile strength of composite aerospace structures after low velocity impact

Author:

Cestino E.ORCID,Romeo G.,Piana P.,Danzi F.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference26 articles.

1. Composite Aircraft Structure, AMC 20-29, Acceptable means of compliance, pp. 1–36, European Aviation Safety Agency (2010).

2. Low-velocity impact and residual tensile strength analysis to carbon fiber composite laminates;Wang;Mater. Des.,2010

3. Residual strength prediction of impacted CFRP laminates;Caprino;J. Compos. Mater.,1984

4. Failure mechanisms on composite specimens subjected to compression after impact;de Freitas;Compos. Struct.,1998

5. Low velocity impact and compression after impact test on thin carbon/epoxy laminates;Ghelli;Composites, Part B,2011

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