Fatigue and fracture assessment of toxic metal replacement coatings for aerospace applications-Reference-Cited by-同舟云学术

Fatigue and fracture assessment of toxic metal replacement coatings for aerospace applications

Published:2010-11 Issue:6 Volume:88 Page:303-310
ISSN:0020-2967
Container-title:Transactions of the IMF
language:en
Short-container-title:Transactions of the IMF

Author:

Cree A. M.,Devlin M.,Critchlow G.,Hirst T.

Publisher

Informa UK Limited

Subject

Metals and Alloys,Surfaces, Coatings and Films,Surfaces and Interfaces,Mechanics of Materials,Condensed Matter Physics

Link

http://www.tandfonline.com/doi/pdf/10.1179/002029610X12734927543067

Reference21 articles.

1. Adhesion in bonded aluminium joints for aircraft construction

2. W. D. J. t'Hart and A. Nederveen: 'The influence of different types of anodic layers on the fatigue properties of 2024-T4 and 7075-T6 sheet material', NLR Report No. TR80077U, National Aerospace Laboratory, Amsterdam, The Netherlands, 1980.

3. R. L. H. Wanhill: 'The effects of cladding and anodising on flight simulation fatigue', NLR Report No. TR85006U, National Aerospace Laboratory, Amsterdam, The Netherlands, 1985.

4. Effect of hard anodize thickness on the fatigue of AA6061 and C355 aluminium

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