Crippling strength of axially loaded rods / by Fr. Natalis.

Format:

Book

Government document

Author/Creator:

Natalis, Friedrich, author.

Contributor:

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

Series:

Technical note (United States. National Advisory Committee for Aeronautics) ; 31.

Technical notes / National Advisory Committee for Aeronautics ; No. 31

Language:

English

Subjects (All):

Bars (Engineering).

Strains and stresses--Mathematical models.

Strains and stresses.

bars (building materials).

Physical Description:

1 online resource (34 pages, 2 unnumbered pages) : illustrations

Place of Publication:

[Washington, D.C.] : National Advisory Committee for Aeronautics, 1921.

Summary:

The formulas employed for calculation of rods subject to compression, are usually of value only for stout or for slender rods. They do not cover, as a rule, the whole range of rod lengths, or they give too great a safety factor for short and moderately large rods. Therefore a new empirical formula (equation 8) has been developed that holds good for any length and any material of the rod, and agrees well with the results of extensive strength tests.

Notes:

Title from title screen (viewed June 20, 2019).

"October, 1921."

"Translated from Technische Berichte, Volume III, No. 6, by F.W. Pawlowski."

No Federal Depository Library Program (FDLP) item number.

Includes bibliographical reference (page 1).

Print version record.

Other Format:

Print version: Natalis, Friedrich. Crippling strength of axially loaded rods

OCLC:

1105635892