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Structural Integrity and Durability of Advanced Composites by Alma Hodzic, Constantinos Soutis, Peter Beaumont

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Index

Note: Page numbers followed by “b”, “f” and “t” indicate boxes, figures and tables respectively.

A
Accumulated load-time model, 608
Adhesives impact
under impact, 603–605
under impact-fatigue, 605–606
impact-fatigue, phenomenological models of, 607–608
modelling impacts in, 606
Adhesive transfers load, 717–720
American Airlines Airbus A300-600, 356–357, 357f
American Society for Testing and Materials (ASTM), 549–550
Armoured (composite) fighting vehicles (AFVs), 357–358, 387
B
Barely visible impact damage (BVID), 550
Bazant’s crack band model, 253–254
Biaxiality ratio, 486
Bidimensional compression, 343, 343f
Boeing’s 787 Dreamliner Wing, 355–356, 356f
Bonded joints, crack propagation in, 285–287, 286f, 287t
Bonding thickness effect, 592
Boundary condition ...

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