Fatigue Crack Growth in 7050T7451 Aluminium Alloy Thick Section ...
Fatigue Crack Growth in 7050T7451 Aluminium Alloy Thick Section ...
Fatigue Crack Growth in 7050T7451 Aluminium Alloy Thick Section ...
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DSTO-TR-1477Barter, S. A., <strong>Fatigue</strong> <strong>Crack</strong> <strong>Growth</strong> <strong>in</strong> <strong>7050T7451</strong> Alum<strong>in</strong>ium <strong>Alloy</strong> <strong>Thick</strong> <strong>Section</strong> Plate with aSurface Condition Simulat<strong>in</strong>g Some Regions of F/A-18 Structure. DSTO-TR-1458, Department ofDefence, Defence Science and Technology Organisation. 2003.Clayton, J. Q. and Clark, G., The effect of Steel Shot and Glass Bead Peen<strong>in</strong>g Treatments on the<strong>Fatigue</strong> Resistance of 7050-T76351 Alum<strong>in</strong>ium <strong>Alloy</strong>, Proc. Aust. Ftact. Group, Fracture Mechanics<strong>in</strong> Eng<strong>in</strong>eer<strong>in</strong>g Practice, Melbourne. pp44-51. 1988.Clark, G., Modell<strong>in</strong>g Residual Stresses and <strong>Fatigue</strong> <strong>Crack</strong> <strong>Growth</strong> at Cold-Expanded FastenerHoles. <strong>Fatigue</strong> Fract. Engng Mater. Struct. Vol. 14, No. 5, pp. 379-589, 1991.Clark, G. and Clayton, J. Q., Effectiveness of Peen<strong>in</strong>g Treatments <strong>in</strong> Improv<strong>in</strong>g <strong>Fatigue</strong> Resistanceof 7050 Alum<strong>in</strong>ium <strong>Alloy</strong> under Constant Amplitude and Spectrum Load<strong>in</strong>g, Aust. Surface EngngConf., University of Sth. Australia, 1991.Miller, K., The Short <strong>Crack</strong> problem., <strong>Fatigue</strong> Fract. Engng Mater. Struct. Vol. 5, No. 3, pp. 223-232.1982.Molent, L., Ogden, R. and Pell, R., F/A-18 FS488 Bulkhead <strong>Fatigue</strong> Coupon Test Program. DSTO-TR-0941, Airframes and Eng<strong>in</strong>es Division, Department of Defence, Defence Science andTechnology Organisation. 2000.Sharp, P. K. and Clark, G., The Effects of Peen<strong>in</strong>g on the <strong>Fatigue</strong> Life of 7050 Alum<strong>in</strong>ium <strong>Alloy</strong>.DSTO-RR-0208, AR N0. 011-795, Department of Defence, Defence Science and TechnologyOrganisation. 2001.Sharp, P. K, Byrnes, R. and Clark, G., Exam<strong>in</strong>ation of 7050 <strong>Fatigue</strong> <strong>Crack</strong> <strong>Growth</strong> Data and itsEffect on Life Prediction. DSTO-TR-0729, AR-010-648, Department of Defence, Defence Scienceand Technology Organisation. 1998.Sharp, P. K, Clayton, J. Q. and Clark, G., The <strong>Fatigue</strong> Resistance of Peened 7050-T7451 Alum<strong>in</strong>ium<strong>Alloy</strong> – Repair and Re-Treatment of Component Surface, <strong>Fatigue</strong> Fract. Eng Mater Structure. Vol17, No3, pp243-252. 1994.Simpson, D.L., Molent, L., Landry, N., Roussel, J., Graham, A.D. and Schmidt, N., “The Canadianand Australian F/A-18 International Follow-On Structural Test Project”, Proc. ICAS 2002Congress, Toronto, Canada. 2002.Wang, C. H., Barter, S. A. and Liu, Q., A Closure Model to <strong>Crack</strong> <strong>Growth</strong> Under Large-ScaleYield<strong>in</strong>g and Through Residual Stress Fields. Journal of Eng<strong>in</strong>eer<strong>in</strong>g Material and Technology,Vol. 125. 2003.35
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