Acoustic Fatigue: A method of calculating the fatigue life of a panel subject to jet noise for aircraft ground and flight conditions

Abstract

IN order to prevent acoustic fatigue cracks occurring in structure subjected to jet noise the various airworthiness authorities are proposing to lay down appropriate design criteria. It may not be long therefore before airframe manufacturers are required to show to airworthiness authorities that either:

Citation

Townsend, N.A. (1966), "Acoustic Fatigue: A method of calculating the fatigue life of a panel subject to jet noise for aircraft ground and flight conditions", Aircraft Engineering and Aerospace Technology, Vol. 38 No. 7, pp. 8-10. https://doi.org/10.1108/eb034163