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Consider the metal specimen described in Problem 11 above (KIC =64 MPa-sqrt(m); edge crack measures 7.074...

Consider the metal specimen described in Problem 11 above (KIC =64 MPa-sqrt(m); edge crack measures 7.074 mm; Y = 1.2; Paris’ m = 1.9 and Paris’ A = 2.3E-12 meters / (cycle-MPa-sqrt(m)) ^1.9).    Use Excel and Goal Seek to estimate the cyclic tensile stress amplitude that results in fatigue life of 47.932E6 cycles.

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