Paper Title:
Targeting Problems of Composite Failure
  Abstract

Predicting precisely where a crack will develop in a material under stress and exactly when in time catastrophic fracture of the component will occur is one the oldest unsolved mysteries in the design and building of large-scale engineering structures. Fitness considerations for long-life implementation of aerospace composites include understanding phenomena such as fatigue, creep and stress corrosion cracking that affect reliability, life expectancy, and durability of structure. Structural integrity analysis treats the design, the materials used, and figures out how best components and parts can be joined; furthermore, SI takes into account service duty.

  Info
Periodical
Key Engineering Materials (Volumes 417-418)
Edited by
M.H Aliabadi, S. Abela, S. Baragetti, M. Guagliano and Han-Seung Lee
Pages
37-40
DOI
10.4028/www.scientific.net/KEM.417-418.37
Citation
P. W.R. Beaumont, "Targeting Problems of Composite Failure", Key Engineering Materials, Vols. 417-418, pp. 37-40, 2010
Online since
October 2009
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Price
$32.00
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