H.H. Bryan, K.K. Ahuja

This paper reviews the theories and research currently available on crack propagation under unsteady loadings, especially those of acoustic origin. Since the original theories on fatigue failure did not account for random loading conditions, modified theories which provide statistical methods for evaluating the random loading have emerged. With the recent upsurge in interest in high speed vehicles, the need for understanding fatigue under unsteady loading has become quite critical. In this review, the research on acoustic fatigue failure, conducted primarily over the last forty years, is presented.

DGLR/AIAA 14th Aeroacoustics Conference, 1992

Conference Paper

englisch

21,0 x 29,7 cm, 12 Seiten

DGLR-Bericht, 1992, 1992-03, DGLR/AIAA 14th Aeroacoustics Conference - Proceedings; S.767-778; 1992; Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn

NA

aeroacoustics, crack propagation

Bibliothek

1992