VM-WB-MECH-082

VM-WB-MECH-082
Fracture Mechanics Stress for a Crack in a Plate

Overview

Reference:

Brown, W. F., Jr., & Srawley, J. E. (1966). Plane strain crack toughness testing of high strength metallic materials. ASTM STP-410.

Solver(s):

Ansys Mechanical

Analysis Type(s):Static Structural Analysis
Element Type(s):Solid

Test Case

A long plate with a center crack is subjected to an end tensile stress 0 as shown in problem sketch. Symmetry boundary conditions are considered and the fracture mechanics stress intensity factor KI is determined.

This problem is also presented in

VM256

in the Mechanical APDL Verification Manual.

Figure 107: Schematic

Schematic
Schematic

Material PropertiesGeometric PropertiesLoading

E = 30 x 106 psi

ν = 0.3

a = 1 in

b = 5 in

h = 5 in

t = 0.25 in”

σ0 = 0.5641895 psi

Results Comparison

ResultsTargetMechanicalError (%)
Stress Intensity KI1.02491.04952.4