Accession Number:

AD0763643

Title:

Random Load Fatigue.

Descriptive Note:

Conference proceedings no. 118,

Corporate Author:

ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT PARIS (FRANCE)

Personal Author(s):

Report Date:

1973-06-01

Pagination or Media Count:

13.0

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.

Subject Categories:

  • Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE