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A specimen of a 4340 steel alloy with a plane strain fracture toughness of 54.8 MPa m (50 ksi in. ) is exposed to a stress of 1090 MPa (158100 psi). Assume that the parameter Y has a value of 1.11. (a) If the largest surface crack is 0.8 mm (0.03150 in.) long, determine the critical stress σc.

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To solve this problem it is necessary to apply the concepts related to stress failure, stress and last module Young.

Critical stress by definition is given as,


\sigma_c = (K_(IC))/(Y√(\pi a))

Where,


K_(IC) =Strain fracture toughness

Y = Young's module

a = Length surface crack

Our values are given as,


K_(IC) = 54.8Mpa


Y = 1.11


a = 0.8*10^(-3)m

Replacing in our previous equation we have,


\sigma_c = \frac{54.8}{(1.11)\sqrt{\pi(0.8*10^(-3))}}


\sigma_c = 984.77Mpa

Therefore the critical stress is 984.77Mpa

User Roland Franssen
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