A platform for research: civil engineering, architecture and urbanism
The lead crack concept applied to defect growth in aircraft composite structures
The lead crack concept applied to defect growth in aircraft composite structures
The lead crack concept applied to defect growth in aircraft composite structures
Molent, L. (author) / Forrester, C. (author)
Composite structures ; 166 ; 22-26
2017-01-01
5 pages
Article (Journal)
English
DDC:
624.18
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
A stochastic crack growth analysis for aircraft structures
British Library Conference Proceedings | 1993
|The equivalent elastic crack concept as applied to axisymmetric crack problems
British Library Online Contents | 1998
|Fatigue crack growth history in damage tolerance design of aircraft structures
British Library Online Contents | 2009
|Built-In Diagnostics for Monitoring Crack Growth in Aircraft Structures (Keynote Presentation)
British Library Online Contents | 2001
|Innovative laser heating methodology study for crack growth retardation in aircraft structures
British Library Online Contents | 2005
|