Nonlinear acoustics and honeycomb materials

dc.contributor.author Thompson, Donald
dc.contributor.department Center for Nondestructive Evaluation
dc.date 2018-02-13T06:06:47.000
dc.date.accessioned 2020-06-30T01:25:27Z
dc.date.available 2020-06-30T01:25:27Z
dc.date.copyright Sun Jan 01 00:00:00 UTC 2012
dc.date.embargo 2013-02-11
dc.date.issued 2011-07-01
dc.description.abstract <p>The scope of research activity that Bruce Thompson embraced was very large. In this talk three different research topics that the author shared with Bruce are reviewed. They represent Bruce's introduction to NDE and include nonlinear acoustics, nondestructive measurements of adhesive bond strengths in honeycomb panels, and studies of flexural wave dispersion in honeycomb materials. In the first of these, four harmonics of a 30 Mhz finite amplitude wave were measured for both fused silica and aluminum single crystals with varying lengths and amounts of cold work using a capacity microphone with heterodyne receiver with a flat frequency response from 30 to 250 Mhz. The results for fused silica with no dislocation structure could be described by a model due to Fubini, originally developed for gases, that depends upon only the second and third order elastic constants and not the fourth and higher order constants. The same was not true for the aluminum with dislocation structures. These results raised some questions about models for harmonic generation in materials with dislocations. In the second topic, experiments were made to determine the adhesive bond strengths of honeycomb panels using the vibrational response of the panels (Chladni figures). The results showed that both the damping characteristics of panel vibrations as a whole and velocity of propagation of elastic waves that travel along the surface and sample the bondline can be correlated with destructively determined bond strengths. Finally, the phase velocity of flexural waves traveling along a 1-inch honeycomb sandwich panel was determined from 170 Hz to 50 Khz, ranging from 2.2×10<sup>4</sup> cm/sec at the low end to 1.18×10<sup>5</sup> cm/sec at 40 Khz. The dispersion arises from the finite thickness of the panel and agreed with the results of continuum models for the honeycomb. Above 40 Khz, this was not the case. The paper concludes with a tribute to Bruce for his many wonderful contributions and lessons beyond his technical legacy for all of us.</p>
dc.description.comments <p>Copyright 2012 American Institute of Physics. This article may be downloaded for personal use only. Any other use requires prior permission of the author and the American Institute of Physics.</p> <p>This article appeared in <em>AIP Conference Proceedings </em>1430 (2012): 16–27 and may be found at <a href="http://link.aip.org/link/doi/10.1063/1.4716452">h</a><a href="http://link.aip.org/link/doi/10.1063/1.4716211">http://dx.doi.org/10.1063/1.4716211</a>.</p>
dc.identifier archive/lib.dr.iastate.edu/cnde_conf/23/
dc.identifier.articleid 1038
dc.identifier.contextkey 3684660
dc.identifier.s3bucket isulib-bepress-aws-west
dc.identifier.submissionpath cnde_conf/23
dc.identifier.uri https://dr.lib.iastate.edu/handle/20.500.12876/15640
dc.language.iso en
dc.source.bitstream archive/lib.dr.iastate.edu/cnde_conf/23/2011_Thompson_NonlinearAcousticsHoneycomb.pdf|||Fri Jan 14 22:45:18 UTC 2022
dc.subject.disciplines Materials Science and Engineering
dc.subject.keywords acoustic emission testing
dc.subject.keywords adhesion
dc.subject.keywords adhesive bonding
dc.subject.keywords condition monitoring
dc.subject.keywords damping
dc.subject.keywords elastic waves
dc.subject.keywords honeycomb structures
dc.subject.keywords nondestructive testing
dc.subject.keywords sandwich structures
dc.subject.keywords structural engineering
dc.subject.keywords structural panels
dc.subject.keywords vibrations
dc.subject.keywords nondestructive evaluation
dc.subject.keywords QNDE
dc.title Nonlinear acoustics and honeycomb materials
dc.type article
dc.type.genre conference
dspace.entity.type Publication
relation.isOrgUnitOfPublication f2b877c3-5654-4c6a-9e64-6c944f9f02b6
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