An Exploratory Study of Damage Accumulation Methods for Propagating Fatigue Cracks.
Abstract
This report presents three methods that predict damage/accumulation and crack initiation lives for notched laboratory specimens that were subjected to stepwise increasing load. Constant load amplitude and monotonic tensile tests provide the necessary baseline data for establishing the relationship between cyclic loads applied and the damage accumulation process.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 01, 1978
- Accession Number
- ADA366460
Entities
People
- G. W. Trickle
- H. D. Stalnaker
- J. E. Grove
- J. F. Gallagher
- R. A. Kleismit
Organizations
- Flight Dynamics Laboratory