Effect of normal pressure on the critical compressive stress of curved sheet /

Bibliographic Details
Main Author:	Rafel, Norman
Corporate Authors:	Knovel (Firm), United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Format:	eBook
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, [1942]
Series:	Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L258.
Subjects:	Atmospheric pressure. Buckling (Mechanics) Strains and stresses. Loads (Mechanics) Charts, diagrams, etc. Electronic books.
Online Access:	Connect to the full text of this electronic book

Description
Abstract:	Results are presented of tests of two specimens tested to study the effect of normal pressure on the critical compressive stress for thin curved sheets. These specimens are designated by their respective rib spacings of 10 inches and 30 inches. The relationship between compressive stress and normal pressure at which buckles disappeared is independent of whether the buckles were made to disappear by increase of normal pressure or decrease of compressive stress.
Item Description:	NACA Wartime Report L-258. Originally issued as NACA as a Restricted Bulletin (November 1942). Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia. Electronic resource.
Physical Description:	1 online resource (2 pages, 8 unnumbered pages) : illustrations.
ISBN:	9781680156348 1680156349