Critical combinations of shear and direct axial stress for curved rectangular panels
A solution is presented for the problem of the buckling of curved rectangular panels subjected to combinded shear and direct axial stress. Charts giving theoretical critical combinations of shear and direct axial stress are presented for panels having five different length-width ratios.
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Format: | eBook |
Language: | English |
Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1949.
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Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 1928. |
Subjects: | |
ISBN: | 9781680156164 1680156160 |
Physical Description: | 1 online resource (29 pages) : illustrations |
Online Access:
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