Normal pressure was found to make the buckling load larger than its value for zero pressure; the theoretical buckling load was larger by a factor of 3.1 for one combination of axial load and normal pressure. Normal pressure caused a decrease in effective width at loads below the normal buckling load and in increasse in effective width for loads somewhat greater than the normal buckling load; however, normal pressure caused less than 1 percent increase in effective width for average compressive strains greater than six times the buckling strain. for zero normal pressure.
Book Details
- Public Domain: Yes
- Country: US
- Published: 1944
- Publisher: National Advisory Committee for Aeronautics
- Language: English
- Pages: 11
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