Results show that design of joint gives wider range of fatigue strengths than does choice of material; no one sheet alloy showed superiority over others.
Results of shear fatigue tests of joints with 3/16-inch-diameter 24s-T31 rivets in 0.064-inch-thick alclad sheet
Nat Advisory Committee Aeronautics -- Tech Note
1950
45 pages
Illustrations, Diagrams, Charts, Tables
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Fatigue Tests on 1/8-inch Aluminum Alloy Rivets
NTRS | 1945
|Development of Fatigue-Rated 7/16 Inch Diameter Flush-Head Rivets for Aluminum Wing Structure
SAE Technical Papers | 1995
|