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Published in:
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2019 | OriginalPaper | Chapter

3. Fatigue Crack Growth

Authors : Sérgio M. O. Tavares, Paulo M. S. T. de Castro

Published in: Damage Tolerance of Metallic Aircraft Structures

Publisher: Springer International Publishing

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Abstract

Readers of this book will have previous knowledge of fracture mechanics, and as such no effort will be made to delve here into fundamental concepts.

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Footnotes
1
English translation in 2011: D. Gross, T. Seelig, ‘Fracture Mechanics: with an Introduction to Micromechanics’, Springer, 2011.
 
2
English translation in 2016: H. A. Richard, M. Sander, ‘Fatigue Crack Growth: Detect—Assess—Avoid’, Springer, 2016.
 
3
English version in 2016: J. T. P. de Castro, M. A. Meggiolaro, ‘Fatigue Design Techniques’, 3 vols., CreateSpace, 2016.
 
Literature
1.
C. Dharan, B. Kang, I. Finnie, Finnie’s Notes on Fracture Mechanics, (Springer Science+Business Media, 2016)
2.
A.T. Zehnder, Fracture Mechanics (Springer Science+Business Media, 2012 )
3.
T.L. Anderson, Fracture Mechanics: Fundamentals and Applications, 4th edn. (CRC Press, 2017)
4.
E.E. Gdoutos, Fracture Mechanics: An Introduction (Springer, 2005)
5.
P.P. Milella, Fatigue and Corrosion in Metals (Springer, 2013)
6.
D. Gross, T. Seelig, Bruchmechanik: mit einer Einführung in die Mikromechanik, 6th edn. (Springer-Verlag, 2016)
7.
H.A. Richard, M. Sander, Ermüdungsrisse: Erkennen, sicher beurteilen, vermeiden (Springer, 2009)
8.
J.T.P. de Castro, M.A. Meggiolaro, Fadiga: Técnicas e Práticas de Dimensionamento Estrutural sob Cargas Reais de Serviço, Volume I - Iniciação de Trincas; Volume II - Propagação de Trincas, Efeitos Térmicos e Estocásticos (CreateSpace Independent Publishing Platform, 2009)
9.
A. Arteiro, P.M.S.T. de Castro, Mecânica da Fratura e Fadiga: Exemplos de Cálculo e Aplicação (FEUP edições, 2014)
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J.W. Bristow, P.E. Irving, Safety factors in civil aircraft design requirements. Eng. Fail. Anal. 14, 459–470 (2007)CrossRef
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S.M.O. Tavares, P.M.S.T. de Castro, Fatigue crack growth of aircraft structures: sensitivity to materials parameters. Int. J. Terraspace Sci. Eng. 6(2), 71–75 (2014)
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R. Jones, Fatigue crack growth and damage tolerance. Fatigue Fract. Eng. Mater. Struct. 37(5), 463–483 (2014)CrossRef
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J. Ge, Y. Sun, S. Zhou, L. Zhang, Y. Zhang, Q. Zhang, A hybrid frequency-time domain method for predicting multiaxial fatigue life of 7075–T6 aluminium alloy under random loading. Fatigue Fract. Eng. Mater. Struct. 38, 247–256 (2015)CrossRef
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C.V. Haden, D.G. Harlow, Statistical characterization of the geometric properties of particles in 7075–T6 aluminium alloy. Fatigue Fract. Eng. Mater. Struct. 37, 1281–1290 (2014)CrossRef
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P. Heuler, H. Klätschke, Generation and use of standardised load spectra and load-time histories. Int. J. Fatigue 27(8), 974–990 (2005)CrossRef
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Fatigue technology—FTI, Tooling Catalog. Revision 7 (Seattle, WA, USA, 2014)
17.
P.F.P. de Matos, P.M.G.P. Moreira, P.P. Camanho, P.M.S.T. de Castro, Numerical simulation of cold working of rivet holes. Finite Elem. Anal. Des. 41(9–10), 989–1007 (2005)CrossRef
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Y. Fu, E. Ge, H. Su, J. Xu, R. Li, Cold expansion technology of connection holes in aircraft structures: a review and prospect. Chin. J. Aeronaut. 28(4), 961–973 (2015)CrossRef
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D.L. Andrew, P.N. Clark, D. Hoeppner, Investigation of cold expansion of short edge margin holes with pre-existing cracks in 2024–T351 aluminium alloy. Fatigue Fract. Eng. Mater. Struct. 37, 406–416 (2014)CrossRef
20.
G.M. Vallières, D.L. DuQuesnay, Fatigue life of cold-expanded fastener holes with interference-fit fasteners at short edge margins. Fatigue Fract. Eng. Mater. Struct. 38(2015), 574–582 (2015)CrossRef
21.
A. Ali, X. An, C.A. Rodopoulos, M.W. Brown, P. Ohara, A. Levers, S. Gardiner, The effect of controlled shot peening on the fatigue behaviour of 2024–T3 aluminium friction stir welds. Int. J. Fatigue 29(8), 1531–1545 (2007)CrossRef
22.
G. Ivetic, (guest-editor), Special issue: advances in laser shock peening theory and practice around the world—present solutions and future challenges. Int. J. Struct. Integr. 2(1) (2011)
23.
C.A. Rodopoulos, J. Bridges, The use of ultrasonic impact treatment to extend the fatigue life of integral aerospace structures, in Engineering Against Fracture: Proceedings of the 1st Conference, ed. by S. Pantelakis, C. Rodopoulos (Springer, 2009), pp. 421–430
24.
R. Jones, N. Matthews, C.A. Rodopoulos, K. Cairns, S. Pitt, On the use of supersonic particle deposition to restore the structural integrity of damaged aircraft structures. Int. J. Fatigue 33, 1257–1267 (2011)CrossRef
25.
R. Jones, L. Molent, S. Barter, N. Matthews, D. Tamboli, Supersonic particle deposition as a means for enhancing the structural integrity of aircraft structures. Int. J. Fatigue 68, 260–268 (2014)CrossRef
26.
N. Matthews, R. Jones, G.C. Sih, Application of supersonic particle deposition to enhance the structural integrity of aircraft structures. Sci. China: Phys. Mech. Astron. 57(1), 12–18 (2014)
27.
Congressional Record-House, Conference report on H.R. 4546, Bob Stump National Defense Authorization Act for Fiscal Year 2003 (see: Sec. 1067. Prevention and mitigation of corrosion of military equipment and infrastructure.) (2002) pp. H8092–H8535
28.
US Department of Defense—DoD, Corrosion prevention and mitigation strategic plan. September 2011
Metadata
Title
Fatigue Crack Growth
Authors
Sérgio M. O. Tavares
Paulo M. S. T. de Castro
Copyright Year
2019
Book
Damage Tolerance of Metallic Aircraft Structures

Print ISBN: 978-3-319-70189-9

Electronic ISBN: 978-3-319-70190-5

Copyright Year: 2019

DOI
https://doi.org/10.1007/978-3-319-70190-5_3

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