Some tests on the effect of fatigue loading on the friction in riveted light alloy specimens

Title

Some tests on the effect of fatigue loading on the friction in riveted light alloy specimens

 Author

Hartman, A.

Institution

National Aerospace Laboratory NLR

 Date

1961-03-30

 Abstract

Single row riveted double cover plate joints in alclad 2024-T aluminium alloy sheet and 2117-T snap rivets were loaded in fluctuating tension with cycle ratio's from 0.25 to 0,79. The specimens were then tested by a static rotation test to determine the effect of the pre-loading in fatigue on the friction between the sheets. The friction had increased by a factor of about three, which value had been attained already at a cycle ratio of 0.25

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 Publisher

Nationaal Lucht- en Ruimtevaartlaboratorium

 Access restriction

Campus only

 Source

NLR TM-M.2088

 Part of collection

Aerospace Engineering Reports

 Document type

report

 Rights

(c) 1961 National Aerospace Laboratory NLR
Files
PDF NLR-TM.M.2088.pdf 18.21 MB
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