Calculations for a single-strut biplane with reference to the tensions in the wing bracing / by O. Blumenthal.

Format:

Book

Government document

Author/Creator:

Blumenthal, Otto, 1876-1944, author.

Contributor:

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

Series:

Technical note (United States. National Advisory Committee for Aeronautics) ; 143.

Technical notes / National Advisory Committee for Aeronautics ; No. 143

Language:

English

Subjects (All):

Airplanes--Wings.

Airplanes.

Strains and stresses.

Struts (Engineering).

Mathematical models.

Models, Theoretical.

mathematical models.

Medical Subjects:

Models, Theoretical.

Physical Description:

1 online resource (28 pages, 3 unnumbered pages) : illustrations.

Place of Publication:

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

Summary:

Since the influence of the initial tensions in the wing bracing on the stressing of airplane parts does not yet appear to have been sufficiently elucidated, an example will be worked out below for a heavily staggered biplane with a single rigid outer strut.

Notes:

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

"June 1923."

"From Technische Berichte, Vol. III, No. 5."

"Translated by National Advisory Committee for Aeronautics"--Page 28.

No Federal Depository Library Program (FDLP) item number.

Includes bibliographical references.

Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.

Other Format:

Print version: Blumenthal, Otto, Calculations for a single strut biplane with reference to the tensions in the wing bracing

OCLC:

1117765907