Residual life prediction for surface cracks in complex structural details
Author:
Affiliation:
1. Pratt & Whitney Aircraft Division, United Aircraft Corporation, East Hartford, Conn.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.44458
Reference9 articles.
1. Numerical solutions in three dimensional elastostatics
2. An improved boundary-integral equation method for three dimensional elastic stress analysis
3. On the finite element method in linear fracture mechanics
4. The distribution of stress in the neighbourhood of a flat elliptical crack in an elastic solid
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