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Effect of Rivet Pitch upon the Fatigue Strength of Single-row Riveted Joints of 0.025- to 0.025-inch 24S-T AlcladS-N curves at the range ratio of 0.2 were experimentally obtained for each of the following values of rivet pitch P as used in a single-row lap joint of 0.025- to 0.025-inch 24S-T alclad with one-eight AN430 round-head rivets: p=0.5, 0.75, 1.0, 1.5. Families of constant rivet pitch curves, which define the fatigue life for specimens studied, were developed. Curves showing the variation of the effective stress concentration factor in fatigue with rivet pitch and maximum load per rivet were also established.
Document ID
19930081607
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Seliger, Victor
(Lockheed Aircraft Corporation)
Date Acquired
September 6, 2013
Publication Date
July 1, 1943
Report/Patent Number
NACA-TN-900
Report Number: NACA-TN-900
Accession Number
93R10897
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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