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Experimental stress analysis of stiffened cylinders with cutouts.pure torsion
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1953 |
| Description | Torsion tests were made on a cylindrical semimonocoque shell of circular cross section. The cylinder was first tested without a cutout, and then with a rectangular cutout which was successively enlarged through six sizes varying from 30 degrees to 130 degrees in circumference and from 1 to 2 bays in length. Strain measurements were made with resistance-type wire strain gages near the cutout on the stringers, the skin, and the rings for each size of cutout, and the stresses obtained are presented in tables. (author) |
| File Size | 12461265 |
| Page Count | 42 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930083677 |
| Archival Resource Key | ark:/13960/t5r82pq1p |
| Language | English |
| Publisher Date | 1953-11-01 |
| Access Restriction | Open |
| Subject Keyword | Loads AND Stresses, Structural - Torsion Loads AND Stresses, Structural Cylinders, Structural - Circular Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
