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

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, a...

Full description

Saved in:
Bibliographic Details
Main Author: Gallaher, George L., (Author)
Corporate Author: United States. National Advisory Committee for Aeronautics.
Other Authors: Boughan, Rolla B.
Format: 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:
ISBN: 9781680156102
1680156101
Physical Description: 1 online resource (15 pages) : illustrations, tables

Cover

Table of contents