Fittings and other structural parts of airplanes / by P. Eydam.

Format:

Book

Government document

Author/Creator:

Eydam, P., author.

Contributor:

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

Series:

Technical note (United States. National Advisory Committee for Aeronautics) ; 160.

Technical notes / National Advisory Committee for Aeronautics ; No. 160

Language:

English

Subjects (All):

Airplanes--Parts--Testing.

Airplanes.

Reliability (Engineering)--Testing.

Reliability (Engineering).

Physical Description:

1 online resource (12 pages, 7 unnumbered pages) : illustrations

Place of Publication:

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

Summary:

The strength and reliability of airplanes depend greatly on the careful design and manufacture of the fittings, couplings and other highly stressed parts. In designing these parts, attention must be paid to the possibility of supplementary stresses, which in certain cases are engendered only by alterations in form during flight or during the loading tests.

Notes:

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

"October 1923."

"From Technische Berichte, Vol. III, No. 6."

"Translated by National Advisory Committee for Aeronautics"--Page 12

No Federal Depository Library Program (FDLP) item number.

Includes bibliographical reference (page 1).

Print version record.

Other Format:

Print version: Eydam, P. Fittings and other structural parts of airplanes

OCLC:

1117765711