Impact damage prediction and failure analysis of heavily loaded, blade-stiffened composite wing panels

Author:

Wiggenraad J.F.M,Zhang X,Davies G.A.O

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference16 articles.

1. Frame CS. Design methodology for the improvement of damage tolerance within composite materials. Brite Euram Contract BREU/0276/C, 1993

2. McCarty JW, Roesseler WG. Durability and damage tolerance of large composite primary aircraft structure. NASA CR-003767, 1984

3. Miller AG, Lovell DT, Seferis JC. The evolution of an aerospace material: influence of design, manufacturing and in-service performance. Composite Structures 1994;27:1, 2

4. Labonté S, Wiggenraad JFM. Development of a structure relevant specimen for damage tolerance studies. In Ninth International Conference on Composite Materials. Madrid, Spain, 1993

5. Labonté S, Wiggenraad JFM. A damage tolerance study conducted with structure relevant specimens. NLR TP 93067 U, 1993

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