Random Load Fatigue.
Abstract
The report briefly discusses the papers given at the conference. The titles of the papers are: A short survey on possibilities of fatigue life assessment of aircraft structures based on random or programmed fatigue tests; Some effects of change in spectrum severity and spectrum shape on fatigue behaviour under random loading; The accumulation of fatigue damage in aircraft materials and structures; Effects of test frequency on fatigue crack propagation under flight-simulation loading; Correlation between laboratory tests and service experience; On residual stresses during random load fatigue; The fatigue life under three different load spectra - tests and calculations; A relation between measured C. G. vertical accelerations and loads at the T-tail of a military airplane.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 01, 1973
- Accession Number
- AD0763643
Entities
People
- Walter Schutz
Organizations
- AGARD