FATIGUE CRACK PROPAGATION IN ALUMINUM-LITHIUM ALLOY 2090: PART I. LONG CRACK BEHAVIOR.

In part I, the crack growth and crack shielding behavior of long ( APP GRTH 5 mm) through thickness cracks is examined as a function of plate orientation and load ratio and compared to high strength aluminum alloys. It is shown that rates of fatigue crack extension in 2090 are, in general, slower (at a given stress intensity range) than in traditional alloys, although behavior is strongly anisotropic. Differences in growth rates of up to 4 orders of magnitude are observed between the L-T, T-L, and T-S orientations which show the best crack growth resistance and the S-L, S-T, and L plus 45 which show the worst. Such behavior is attributed to the development of crack tip shielding (i. e. , a reduction in local crack driving force) primarily resulting from the role of the crack path morphology in inducing crack deflection and crack closure from the consequent asperity wedging. Whereas crack advance perpendicular to the rolling plane (e. g. , L-T, etc. ) involves marked crack path deflection and branching thereby promoting high levels of shielding to cause the slowest growth rates, fatigue fractures parallel to the rolling plane (e. g. , S-L, etc. ) occur by an intergranular, delamination-type separation, with lower shielding levels to give the fastest growth rates.