## Cumulative Fatigue Darnaae Due to Vi 4 Presented at Z9 Symposium on S5hock, Vibration and 'A'e

- J. B. Fuller
- 1960

The stress in aircraft structure resulting from multi-mode response to sonic excitation is resolved into an alternating stress component superimposed upon a slowly varying mean stress component. It is then found that the probability distribution of those components is nearly independent of the number of modes participating in the response. This finding… (More)

@inproceedings{FATIGUESoAO,
title={So ASPECTS OF THE RESPONSE OF STRUCTURES SUBJECT TO SONIC FATIGUE},
author={SONIC FATIGUE}
}