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.
Consider the metal specimen described in Problem 11 above (KIC =64 MPa-sqrt(m); edge crack measures 7.074...
Consider the metal specimen with KIC =64 MPa-sqrt(m); edge crack measures 15.398 mm; Y = 1.05; Paris’ m = 3.1 and Paris’ A = 3.2E-12 meters / (cycle-MPa-sqrt(m)) ^3.1). Use Excel and Goal Seek to estimate the cyclic tensile stress amplitude that results in fatigue life of 0.534E6 cycles.
Consider the metal specimen with KIC =64 MPa-sqrt(m); edge crack measures 15.398 mm; Y = 1.05; Paris’ m = 3.1 and Paris’ A = 3.2E-12 meters / (cycle-MPa-sqrt(m)) ^3.1). Use Excel and Goal Seek to estimate the cyclic tensile stress amplitude that results in fatigue life of 0.534E6 cycles.
Consider the metal specimen described in Problem 11 above (KIC =58 MPa-sqrt(m); edge crack measures 9.711 mm; Y = 1.1; Paris’ m = 3.1 and Paris’ A = 1.7E-12 meters / (cycle-MPa-sqrt(m)) ^3.1). Use Excel and Goal Seek to estimate the cyclic tensile stress amplitude that results in fatigue life of 1.714E6 cycles.
Consider 7075-T6 aluminum with fatigue crack growth in
Table
16. Consider 7075-T6 aluminum with fatigue crack growth properties as given in Table 6.3. Assuming that 1=0.5 in the Walker equation, @. estimate da/dN versus AK equations in the form of Eq. 6.22a for R=0.4 and 0.8. 6. plot the equations from (a) on a log-log scale along with the R=0 equation. Keep in mind the proper region I limits of the equation. 169x10-5 ©. For a given AK, by what...