The strength and stiffness of shear webs with and without lightening holes /

Bibliographic Details
Main Author:	Kuhn, Paul (Author)
Corporate Authors:	Knovel (Firm), United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Format:	Government Document eBook
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, [1942]
Series:	Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L402.
Subjects:	Aluminum alloys. Holes. Shear (Mechanics) Strength of materials. Strains and stresses. Monocoque construction. Charts, diagrams, etc. Electronic books.
Online Access:	Connect to the full text of this electronic book

Description
Abstract:	Nearly 200 tests were made on the strength of shear webs of 24S-T aluminum alloy, with and without lightening holes. The tests were made in a jig of the single-specimen type, in which the specimen is free to collapse completely without developing diagonal tension. The lightening holes were circular and had either flanged edges or beaded edges, the specimens with flanged edges constituting by far the largest test group.
Item Description:	NACA Wartime Report L-402. Originally issued as NACA as an Advance Restricted Report (June 1942). Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia.
Physical Description:	1 online resource (29 pages, 15 unnumbered pages) : illustrations.
Bibliography:	Includes bibliographical references.
ISBN:	9781680156539 1680156535