The effects of stress ratio (R) and crack-opening behavior on fatigue crack growth rates (da/dN) for Aluminum Alloy (AA) 2024-T3 were investigated using constant-ΔK testing, closure measurements, and fractography. Fatigue crack growth rates were obtained for a range of ΔK and stress ratios. Results show that constant ΔK fatigue crack growth for R ranging from near 0 to near 1 is divided into three regions. In Region I, at low R, da/dN increases with increasing R. In Region II, at intermediate R, fatigue crack growth rates are relatively independent of R. In Region III, at high R, further increases in da/dN are observed with increasing R. Near-crack-tip surface closure measurements, using a new noncontact displacement method, show that Region I transient crack growth rates are a result of crack closure. Increasing fatigue surface microvoid density, coinciding with increasing da/dN for Region III fatigue crack growth, suggests that a Kmax-dependent damage mechanism is responsible for the transient fatigue crack growth rates characteristic of Region III. For AA 2024-T3, the onset of Region III correlates with a critical value of Kmax (13 MPa m1/2). Region II fatigue crack growth is unaffected by both closure and Kmax effects. In this intrinsic region, ΔK = ΔKeff Rates from this region are used to test the validity of closure measurements for Region I fatigue crack growth. Poor correlation of da/dN and ΔKeff occurs when ΔKeff is calculated from the fully open load obtained by the reduced strain technique. Good correlation of da/dN and ΔKeff are found when ΔKeff is calculated from local opening loads approximately 0.1 mm behind the crack-tip.
|NASA Technical Memorandum
|Published - 1998
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