An Applied Method for Predicting the Load-Carrying Capacity in Compression of Thin-Wall Composite Structures with Impact Damage

Author:

Mitrofanov O.,Pavelko I.,Varickis S.,Vagele A.

Publisher

Springer Science and Business Media LLC

Subject

Polymers and Plastics,Mechanics of Materials,Condensed Matter Physics,General Mathematics,Biomaterials,Ceramics and Composites

Reference24 articles.

1. AC 20-107B. Composite Aircraft Structure, Sept. 8 (2009).

2. M. E. Waddoups, J. R. Eisenmann, and B. E. Kaminski, “Macroscopic fracture mechanics of advanced composite materials,” J. Compos. Mater., 5, 446-454 (1971).

3. J. P. Trunin, and A. E. Ushakov, “Some questions on the evaluation and maintenance of operational survivability of airframe structures made of composite materials,” Proekt. Rash. Ispyt. Konstr. Kompoz. Mater., TsAGI, X, 84-89 (1984).

4. J. P. Trunin, R. I. Tchizhov, and A. S. Shishmareva, “Investigation of the strength of damaged composite materials and their spot-connected joints in tension, compression, and shear,” TsAGI, No. 2, 48-50 (1982).

5. A. E. Ushakov, Methodology for Ensuring the Operational Survivability and Safety of Aircraft Structures Made of Polymer Composite Materials [in Russian], Fizmatlit, Moscow (2012).

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