Experimental investigation of stresses, with particular regard to relation of plate thickness to rivet diameter; test specimen and rivets were of ultralumin, annealable, artificially aging alumin-copper-nickel alloy; closing head is formed under increasing pressure; paper and discussion give suggestions as to proper design of joints. From Jahrbuch der wissenschaftlichen Gesellschaft fuer Luftfahrt, 1929.
Riveted joints in thin plates
Nat. Advisory Committee Aeronautics -- Tech. Memo
1930
15 pages
9 Figs. on Supp. plates
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Engineering Index Backfile | 1945
|Engineering Index Backfile | 1890
The Strength of Riveted Joints
Emerald Group Publishing | 1945
|Frictional strength of riveted joints
Engineering Index Backfile | 1929
|Fatigue Crack Growth in Riveted Joints
British Library Conference Proceedings | 1997
|