Crack Paths 2012

References

[1] V. R A M S A M O O JT.,A. SHUGAR,(2001), International Journal of Fatigue, Vol.

23, p.301.

[2] C. M A D D U R IR,.V. PRAKASH,(2010) International Journal of Mechanical and

Materials Engineering, p.20.

[3] G. BENAMATIM,. AGOSTINI,I. ALESSANDRINAIN DS. STORAI, (1994),

Journal of Nuclear Materials, Vols. 212-215, p.1515.

[4] N. MIURA,Y. TAKAHASHII:nternational Journal of Fatigue, Vol. 28 (2006),

p.1618.

[5] H. E N H OaUnd al, (1993), Acta Metallurgica Sinica Serie A, Vol. 6, N°6, p.373.

[6] E.S. NIKOLIN, G. V. KARPENKO,(1967),Fiziko-Khimicheskaya Mekhanika

Materialov, Vol. 3, N°1, p.63.

[7] V.S. A R A R A W A L(A20,00), 11th Annual AeroMat Conference, Bellevue, W A ,

June 26-29.

[8] R. KINZIE, (2002), Cost of corrosion, The 6th International Conference on Ageing

Aircraft, San Francisco, USA.

[9] D.W.HOEPPNERA,. TAYLOR,V. C H A N D R A S E K A R(A199N9), Books in the

International Committee on Aeronautical Fatigue, (ICAF) series, ICAF20.

[10] N. A. FILHOand al, (2007) Transactions, SMIRT19, Toronto.

[11] H.SEDJAL,F.HELLAL,(2012), Advanced Material Research, Vol. 445, p.929.

[12] J.C. N E W M AJR.,N E.P. PHILLIPS, M.H. SWAIN,(1999), International Journal

of Fatigue, Vol.21, Issue 2, pp.109-119.

[13] P. BOURDETC,. BLANC,G. M A N K O W S K JI. ,GUILLOT,(2006), Journal of

Materials Science Forum, Vols.519-521, p.741.

[14] J. HEATH,Z. STERJOVSKI,S.P. LYNCH,(2010), Procedia Engineering, Vol. 2,

Issue 1, p.1243.

866