Chapter 08, Problem 8.11 A structural component in the form of a wide plate is to...
A structural bridge component in the form of a wide plate is to be fabricated from a steel alloy that has a fracture toughness of 98.9 MPam and yield strength of 860 MPa. The flaw size resolution limit of the flaw detection apparatus is 3.0 mm. If the design stress is one-half of the yield strength and the value of Y is 1.0, determine whether or not a critical flaw for this plate is subject to detection.
A structural component in the shape of a flat plate 25.0 mm thick is to be fabricated from a metal alloy for which the yield strength and plane strain fracture toughness values are 545 MPa and 29.6 MPa-m1/2, respectively. For this particular geometry, the value of Y is 1.3. Assuming a design stress of 0.3 times the yield strength, calculate the critical length of a surface flaw. (in mm) incorrect answer 2.222 mm
A large plate is fabricated from a steel alloy that has a plane strain fracture toughness of 75 MPam (68.25 ksi vin.). If the plate is exposed to a tensile stress of 347 MPa (50330 psi) during use, determine the minimum length of a surface crack that will lead to fracture. Assume a value of 0.94 for Y. mm
Suppose that a wing component on an aircraft is fabricated from an aluminum alloy that has a plane strain fracture toughness of 25 MPa (22.75 ksi). It has been determined that fracture results at a stress of 117 MPa (16970 psi) when the maximum internal crack length is 9.1 mm (0.3583 in.). For this same component and alloy, compute the stress level at which fracture will occur for a critical internal crack length of 5.5 mm (0.2165 in.).