A method of estimating the critical buckling load for structural members / by Eugene E. Lundquist.

Format:

Book

Government document

Author/Creator:

Lundquist, Eugene E., author.

Contributor:

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

Series:

Technical note (United States. National Advisory Committee for Aeronautics) ; 717.

Technical note / National Advisory Committee for Aeronautics ; No. 717

Language:

English

Subjects (All):

Structural design.

Buckling (Mechanics).

Mathematical analysis.

buckling.

warping (structural change).

Physical Description:

1 online resource (25 pages, 11 unnumbered pages) : illustrations

Place of Publication:

Washington [D.C.] : National Advisory Committee for Aeronautics, 1939.

Summary:

The relations between load on the structure and rotation of a joint can be used to estimate the lowest critical load after the equation for neutral stability has been tested for three assumed critical loads, each of which is less than the lowest critical load.

The solutions of six simple problems are included to illustrate the application of the method of estimating critical loads and to reveal certain characteristics of the method that should be known by the practical engineer using it. Four of these problems are concerned with members that lie in the elastic, or long-column, range. The other two problems are concerned with memberes that lie in the short-column range.

Notes:

Online resource, PDF version; title from title page (TRAIL, viewed November 29, 2021).

"July 1939."

"Langley Memorial Aeronautical Laboratory."

No Federal Depository Library Program (FDLP) item number.

Includes bibliographical references (page 25).

Print version record.

Other Format:

Print version: Lundquist, Eugene E. A Method of estimating the critical buckling load for structural members

OCLC:

1154792555