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Title
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Interface Damping At Riveted Joints. Part I - Theoretical Analysis
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Date
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1961
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Index Abstract
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Not Available
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Photo Quality
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Not Needed
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Report Number
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ASD TR 61-467 Part I
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Creator
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Mead, D. J.
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Eaton, D. C. G.
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Corporate Author
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Southampton Univ (United Kingdom)
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Identifier
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AD0270463
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AD0270463
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Distribution Classification
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1
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DTIC Record Exists
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No
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Distribution Change Authority Correspondence
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AFML LTR
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Report Availability
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Full text available
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Date Issued
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1961-09
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Abstract
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In this paper a theoretical examination is made of potential structural damping increments that could be obtained by insertion of a linear visco-elastic interfacial layer between plates of riveted joints. Consideration is given to a lap joint having anti-symmetry about its single rivet, and being subjected to harmonic longitudinal loading. Certain simplifying assumptions have been which effectively reduce the analysis to a one dimensional system. An expression is obtained for the energy dissipated in the layer per cycle of load. The magnitude of this energy dissipation has been computed for a wide range of joint dimensions, dynamic properties of the layer, and rivet stiffnesses. It has been found that as the thickness (or shear modulus) of the layer is varied, a maximum value of the energy dissipation occurs. The conditions for this maximum are examined, and a simple design rule is established whereby the maximum damping may be achieved in a joint using a given material. It is shown that the elastic deformation of the plates has a significant effect only when high values of rivet stiffness the energy dissipation may be found to a sufficient degree of accuracy by neglecting altogether the plate flexibility.
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Publisher
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Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force
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Date Modified
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Scanned by request 11/2/2018 submitted by Vignan's LARA Institute of Technology & Science (University - International)
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Extent
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41
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Laboratory
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Directorate of Materials and Processes
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Contract
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AF 61(052)-332
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DoD Project
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7351 - Metallic Materials
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DoD Task
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73521 - Behavior of Metals
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Distribution Conflict
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No
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Access Rights
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ASTIA release to OTS not authorized.
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Provenance
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Lockheed Martin Missiles & Fire Control
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Type
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report
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Format
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1 online resource