SEDL / STP / STP462-EB / STP32042S



Comparison of Fatigue Lives Under Conventional Program Loading and Digital Random Loading

Jacoby, GH
Head, Deutsche Versuchsanstalt für Luft-und Raumfahrt, Institut für Festigkeit, Mulheim (Ruhr),


Pages: 19    Published: Jan 1970


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Abstract

On the basis of a gust-load distribution, evaluated by applying level crossing-counting method, an 8-step program test and tests with a random sequence of stress cycles were performed. The results of these tests are compared with the results of tests with a random sequence of maxima and minima. The latter are based on a distribution of maxima and minima, which were derived from the gust-load distribution splitted in several stationary Gaussian processes. In further tests, ground-air-ground cycles were included in the study. Programmed and randomized flight-by-flight tests were compared.

The results of the study revealed that in the case of steady mean stress and the applied conditions program loading overestimates life by a factor of about 6. In case of flight-by-flight tests, however, the load-time history (either programmed or randomized) seem to be unimportant.


Keywords:
random processes, load (forces), fatigue (materials), digital techniques, computer programs, flight tests, crack propagation, tests, evaluation

Paper ID: STP32042S
Committee/Subcommittee: E08.05
DOI: 10.1520/STP32042S
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