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...
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Main Author: | |
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Corporate Author: | |
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Format: | eBook |
Language: | English |
Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1947.
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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 |
Online Access:
Online Resources