Detection of Sublayer Fatigue Cracks under Airframe Rivets Wincheski, Buzz Namkung, Min 2018-02-14T08:09:20.000 2020-06-30T06:49:49Z 2020-06-30T06:49:49Z Thu Jan 01 00:00:00 UTC 1998 1998
dc.description.abstract <p>The Rotating Self-Nulling Probe System developed as a part of the National Aeronautics and Space Administration’s Airframe Structural Integrity Program has been shown in the past to provide a quick and reliable method to detect fatigue cracks hidden under airframe rivets [1–3]. The previous research has concentrated on detecting cracks in the top layer of an airframe lap-splice joint, obtaining a 90% probability of detection for 0.032” long top layer fatigue cracks buried under airframe rivets [2,3]. Although this was a major accomplishment, the question of detectability of fatigue cracks in the lower layers of the joint has been left open. In this work the ability of the system to detect second and third layer fatigue cracks will be explored.</p>
dc.format.mimetype application/pdf
dc.identifier archive/
dc.identifier.articleid 3634
dc.identifier.contextkey 5810428
dc.identifier.s3bucket isulib-bepress-aws-west
dc.identifier.submissionpath qnde/1998/allcontent/42
dc.language.iso en
dc.relation.ispartofseries Review of Progress in Quantitative Nondestructive Evaluation
dc.source.bitstream archive/|||Sat Jan 15 00:12:03 UTC 2022
dc.source.uri 10.1007/978-1-4615-5339-7_42
dc.subject.disciplines Electromagnetics and Photonics
dc.title Detection of Sublayer Fatigue Cracks under Airframe Rivets
dc.type event
dc.type.genre article
dspace.entity.type Publication
relation.isSeriesOfPublication 289a28b5-887e-4ddb-8c51-a88d07ebc3f3
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