Tests on riveted joints in sheet duralumin / by H.F. Rettew and G. Thumin.

Format:

Book

Government document

Author/Creator:

Rettew, H. F., author.

Thumin, G., author.

Contributor:

United States. National Advisory Committee for Aeronautics, issuing body.

Series:

Technical note (United States. National Advisory Committee for Aeronautics) ; 165.

Technical notes / National Advisory Committee for Aeronautics ; No. 165

Language:

English

Subjects (All):

Duralumin.

Riveted joints--Testing.

Riveted joints.

duralumin.

Physical Description:

1 online resource (5 pages, 2 unnumbered pages) : illustrations

Place of Publication:

[Washington, D.C.] : National Advisory Committee for Aeronautics, 1923.

Summary:

In this abstract of a thesis (Massachusetts Institute of Technology, Dept. of Mechanical Engineering, June, 1921) twenty-six tension tests on various forms of single-riveted lap-joints was performed. Three thicknesses of duralumin sheet were used, being furnished and riveted by the Engineering Division of the Army Air Service. In making the tests, the slippage of the joints was noted at three points across each joint. In addition, stress-strain curves were obtained for plain tension specimens, and a chemical analysis was made of the sheet. No analysis was made of the rivets which were annealed duralumin with heads formed before riveting.

Notes:

Title from title screen (viewed August 9, 2019).

"November 1923."

"Abstracted and revised by J.G. Lee."

No Federal Depository Library Program (FDLP) item number.

Print version record.

Other Format:

Print version: Rettew, H.F. Tests on riveted joints in sheet duralumin

OCLC:

1117765926