Charts for calculation of the critical compressive stress for local instability of idealized web- and T-stiffened panels /

Bibliographic Details
Main Author:	Boughan, Rolla B.
Corporate Authors:	Knovel (Firm), United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Other Authors:	Baab, George W.
Format:	eBook
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, [1944]
Series:	Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L204.
Subjects:	Aluminum alloys. Plates (Engineering) Strains and stresses. Buckling (Mechanics) Airplanes > Materials. Charts, diagrams, etc. Electronic books.
Online Access:	Connect to the full text of this electronic book

Description
Abstract:	Charts are presented for the calculation of the critical compressive stress - the stress at which local instability occurs - for idealized web- and T-stiffened panels, and examples of the use of the charts are given.
Item Description:	NACA Wartime Report L-204. Originally issued as NACA as Advance Restricted Report L4H29 (August 1944). Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia. Electronic resource.
Physical Description:	1 online resource (8 pages, 6 unnumbered pages) : illustrations.
Bibliography:	Includes bibliographical references.
ISBN:	9781680156492 1680156497