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

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A Method of calculating the compressive stren ...
George L. Gallaher
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December 19, 2022 | History

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

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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.

Publish Date
Language
English
Pages
15

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Edition Availability
Cover of: A Method of calculating the compressive strength of Z-stiffened panels that develop local instability
A Method of calculating the compressive strength of Z-stiffened panels that develop local instability
1947, National Advisory Committee for Aeronautics
in English

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Book Details


Edition Notes

"November 1947."

NACA TN No. 1482.

Includes bibliographical references.

Published in
Washington, D.C
Series
National Advisory Committee for Aeronautics technical note -- number 1482, Technical note (United States. National Advisory Committee for Aeronautics) -- no. 1482.
Other Titles
Technical Report Archive & Image Library (TRAIL)

Classifications

Dewey Decimal Class
624.17765
Library of Congress
TA660.P6

The Physical Object

Pagination
1 online resource (15 pages)
Number of pages
15

ID Numbers

Open Library
OL44477741M
ISBN 10
1680156101
ISBN 13
9781680156102
OCLC/WorldCat
919093676

Source records

marc_columbia MARC record

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