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1996 | OriginalPaper | Buchkapitel

Lamb Wave Propagation in Thermally Damaged Composites

verfasst von : Michael D. Seale, Barry T. Smith

Erschienen in: Review of Progress in Quantitative Nondestructive Evaluation

Verlag: Springer US

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The use of composites in primary and secondary structures of aerospace vehicles is important for increased performance with little weight penalty. Determining the response to thermal damage is necessary for a complete understanding of the total use environment of these materials. The objective of the research presented here is to provide a method of quantifying the amount of thermal damage in composite materials. Components which have non-visible damage, but have degraded performance on the order of several percent, are of interest. At this level of damage the safety margin designed into the structure may be compromised.

Metadaten
Titel
Lamb Wave Propagation in Thermally Damaged Composites
verfasst von
Michael D. Seale
Barry T. Smith
Copyright-Jahr
1996
Verlag
Springer US
DOI
https://doi.org/10.1007/978-1-4613-0383-1_33

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