So ASPECTS OF THE RESPONSE OF STRUCTURES SUBJECT TO SONIC FATIGUE

  • SONIC FATIGUE

Abstract

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)

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Cite this paper

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