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Tests on Stiffened Circular Cylinders
| Content Provider | University of North Texas |
|---|---|
| Author | Holt, Marshall |
| Organization | United States. National Advisory Committee for Aeronautics. |
| Description | "Compressive tests were made of two series of stiffened circular cylindrical shells under axial load. All the shells were 16 inches in diameter by 24 inches in length and were made of aluminum-alloy sheet curved to the proper radius and welded with one longitudinal weld. The ratios of diameter to thickness of shell wall in the two series of specimens were 258 and 572" (p. 1). |
| File Format | |
| Archival Resource Key | ark:/67531/metadc53665 |
| Language | English |
| Publisher Date | 2018-11-09 |
| Access Restriction | Open |
| Subject Keyword | stiffened circular cylinders compressive testing |
| Content Type | Text |
| Resource Type | Report |