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A Method of calculating the compressive strength of Z-stiffened panels that develop local instability /

Bibliographic Details
Main Author: Gallaher, George L. (Author)
Corporate Authors: Knovel (Firm), United States. National Advisory Committee for Aeronautics
Other Authors: Boughan, Rolla B.
Format: Government Document eBook
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1947.
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; no. 1482.
Subjects:
Plates (Engineering)
Strains and stresses.
Buckling (Mechanics)
Mathematical analysis.
Electronic books.
Online Access:Connect to the full text of this electronic book
Description
Abstract:A method, based on the elastic theory for plate buckling and test results for 24S-T aluminum-alloy Z-stiffened panels, is shown for calculating the compressive strength of Z-stiffened panels that develop local instability. This method can be used to calculate the critical compressive stress above, as well as within, the elastic range. For stresses above three-fourths the compressive yield stress the method can be used for the approximate determination of the average compressive stress at maximum load.
Item Description:"November 1947."
NACA TN Number 1482.
Physical Description:1 online resource (15 pages) : illustrations, tables.
Bibliography:Includes bibliographical references.
ISBN:9781680156102
1680156101