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The Load Distribution in Bolted or Riveted Joints in Light-Alloy StructuresThis report contains a theoretical discussion of the load distribution in bolted or riveted joints in light-alloy structures which is applicable not only for loads below the limit of proportionality but also for loads above this limit. The theory is developed for double and single shear joints. The methods given are illustrated by numerical examples and the values assumed for the bolt (or rivet) stiffnesses are based partly on theory and partly on known experimental values. It is shown that the load distribution does not vary greatly with the bolt (or rivet) stiffnesses and that for design purposes it is usually sufficient to know their order of magnitude. The theory may also be directly used for spot-welded structures and, with small modifications, for seam-welded structures, The computational work involved in the methods described is simple and may be completed in a reasonable time for most practical problems. A summary of earlier theoretical and experimental investigations on the subject is included in the report.
Document ID
19990054354
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Vogt, F.
(Royal Aircraft Establishment Farnborough, United Kingdom)
Date Acquired
August 19, 2013
Publication Date
April 1, 1947
Subject Category
Structural Mechanics
Report/Patent Number
NACA-TM-1135
SME-3300
Report Number: NACA-TM-1135
Report Number: SME-3300
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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