Stress and distortion analysis of a swept box beam having bulkheads perpendicular to the spars /

Bibliographic Details
Main Author:	Heldenfels, Richard R. (Author)
Corporate Authors:	Knovel (Firm), United States. National Advisory Committee for Aeronautics
Other Authors:	Zender, George W., Libove, Charles
Format:	Government Document eBook
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, 1950.
Series:	Technical note (United States. National Advisory Committee for Aeronautics) ; no. 2232.
Subjects:	Box beams. Bulkheads. Strains and stressses. Structural analysis (Engineering) Electronic books.
Online Access:	Connect to the full text of this electronic book

Description
Abstract:	A method is presented for the approximate calculation of the stresses and distortions in a box beam representing the main structural component of a swept wing with a carry-through section and with bulkheads perpendicular to the spars. The application of the method is illustrated by a numerical example and its results are compared with previously published test data.
Item Description:	"November 1950." NACA TN Number 2232.
Physical Description:	1 online resource (90 pages) : illustrations.
Bibliography:	Includes bibliographical references.
ISBN:	9781680156188 1680156187