Formulas for the stress analysis of circular rings in a monocoque fuselage / by Roy A. Miller and Karl D. Wood.

Format:

Book

Government document

Author/Creator:

Miller, Roy A., author.

Wood, K. D. (Karl Dawson), 1898-1995, author.

Contributor:

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

Series:

Technical note (United States. National Advisory Committee for Aeronautics) ; 462.

Technical note / National Advisory Committee for Aeronautics ; No. 462

Language:

English

Subjects (All):

Airplanes--Design and construction.

Airplanes.

Monocoque construction.

Strains and stresses--Mathematics.

Strains and stresses.

Mathematics--Formulae.

Mathematics.

formulas (algorithms).

Genre:

Mathematical formulae.

Physical Description:

1 online resource (15 pages, 13 unnumbered pages) : illustrations.

Place of Publication:

[Washington, D.C.] : National Advisory Committee for Aeronautics, [1933]

Summary:

The formulas given in this report provide a simplified method for the stress analysis of fuselage bulkheads that are approximately circular rings of uniform cross section. Complicated load systems acting on a ring can usually be resolved into simplified load systems; and formulas for moment, axial force, and shear for such simplified examples showing the use of this method in practical stress-analysis work are also included.

Notes:

Description based on online resource, PDF version; title from page 1 (TRAIL, viewed January 13, 2021).

June, 1933.

No Federal Depository Library Program (FDLP) item number.

Includes bibliographical references (page 15).

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

Other Format:

Print version: Miller, Roy A. Formulas for the stress analysis of circular rings in a monocoque fuselage

OCLC:

1143006560