Graduate student, School of Aeronautics and Astronautics, Purdue UniversityAnalytical Services and Materials, Inc., West LafayetteHampton, INVA
Senior scientist, Analytical Services and Materials, Inc., Hampton, VA
Senior scientist, NASA Langley Research Center, Hampton, VA
Head, School of Aeronautics and Astronautics, Purdue University, West Lafayette, IN
Pages: 12 Published: Jan 1992
An inverse technique was used to calculate through-thickness fatigue crack closure behavior. The through-thickness variation in crack opening stress-intensity factor was calculated by considering the variation in the three-dimensional stress-intensity factor, the variation in crack growth rate along the crack front, and a relationship between the crack growth rate and effective stress-intensity factor range (da/dN - ΔKeff). The three-dimensional stress-intensity factor variation was obtained from an elastic finite element analysis of specific crack front profiles observed experimentally. The variation in crack growth rate along the crack front was obtained experimentally from comparison of observed crack front changes. The da/dN - ΔKeff relationship was estimated from high stress ratio, constant load amplitude, fatigue crack growth tests. The through-thickness crack opening stress-intensity factor results agreed with crack opening measurements obtained from fatigue striations, near-tip strain gages, and remote strain and displacement gages.
fatigue (materials), crack closure, through-thickness, inverse calculation, fatigue striations, fracture mechanics
Paper ID: STP23696S