Abstract
Fatigue cracks have been found to initiate and grow in the radial direction in many of the annulus shaped components in aging helicopters. Those include some of the most critical components such as the rotor hub, connecting links and pitch shaft, etc. At the present time, detection of such radial fatigue cracks relies mostly on visual inspection. A more systematic, automated, and efficient method to detect these cracks must be developed.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
References
P. B. Nagy, M. Blodgett and M. Golis, NDT & E International, 27, 131 (1994)
I.A. Viktorov, Soviet Physics- Acoustics, 4, 131 (1958)
L.M. Brekhovskihk, Soviet Physics- Acoustics, 13, 462 (1968)
J., Cerv, ACTA Technica Csav, 89 (1988)
J. D. Achenbach, Wave Propagation in Elastic Solids, North-Holland, New York (1984)
Author information
Authors and Affiliations
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 1996 Plenum Press, New York
About this chapter
Cite this chapter
Qu, J., Berthelot, Y., Li, Z. (1996). Dispersion of Guided Circumferential Waves in a Circular Annulus. In: Thompson, D.O., Chimenti, D.E. (eds) Review of Progress in Quantitative Nondestructive Evaluation. Springer, Boston, MA. https://doi.org/10.1007/978-1-4613-0383-1_21
Download citation
DOI: https://doi.org/10.1007/978-1-4613-0383-1_21
Publisher Name: Springer, Boston, MA
Print ISBN: 978-1-4613-8027-6
Online ISBN: 978-1-4613-0383-1
eBook Packages: Springer Book Archive