Interface Damping At Riveted Joints. Part I - Theoretical Analysis

Item

Title
Interface Damping At Riveted Joints. Part I - Theoretical Analysis
Date
1961
Index Abstract
Not Available
Photo Quality
Not Needed
Report Number
ASD TR 61-467 Part I
Creator
Mead, D. J.
Eaton, D. C. G.
Corporate Author
Southampton Univ (United Kingdom)
Identifier
AD0270463
AD0270463
Distribution Classification
1
DTIC Record Exists
No
Distribution Change Authority Correspondence
AFML LTR
Report Availability
Full text available
Date Issued
1961-09
Abstract
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.
Publisher
Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force
Date Modified
Scanned by request 11/2/2018 submitted by Vignan's LARA Institute of Technology & Science (University - International)
Extent
41
Laboratory
Directorate of Materials and Processes
Contract
AF 61(052)-332
DoD Project
7351 - Metallic Materials
DoD Task
73521 - Behavior of Metals
Distribution Conflict
No
Access Rights
ASTIA release to OTS not authorized.
Provenance
Lockheed Martin Missiles & Fire Control
Type
report
Format
1 online resource