Study of the Influence of Metallurgical Factors on Fatigue and Fracture of Aerospace Structural Materials.
Abstract
This report summarizes the results of a two-phase study involving experimental characterization and analytical modeling of fatigue crack tip micromechanics in aerospace structural (Al and Ti) alloys, and identification and modeling of key factors controlling subcritical crack growth and unstable fracture in single crystal nickel-base superalloys. Crack tip opening displacement, the increment of crack advance, and crack tip strain are assumed to be dependent on the formation of slip lines at the crack tip. Slip line length and dislocation density are parameters in the model which are controlled by the microstructure. The model may be used in two ways: to predict the increment of crack growth, if the slip line length is known, or the length of the slip line may be determined if the crack growth increment is measured. Crack tip plasticity data for 7075-T651 is used to evaluate the model, and the results obtained are compatible with the assumptions, and give a value of slip line length which is compatible with the mean free slip length in the material. In the single crystal nickel-base superalloy task, the details of anisotropic fracture mechanics and crack tip stress field solutions have been reviewed.
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 01, 1984
- Accession Number
- ADA140659
Entities
People
- D. L. Davidson
- G. R. Leverant
- J. E. Hack
- J. Lankford
Organizations
- Southwest Research Institute