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The effective width of curved sheet after buckling
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1938 |
| Description | This report describes experiments made for the purpose of ascertaining the effective width of circularly curved sheet under pure flexural stress. A relation for the effective width of curved sheets is established. Experiments were made with circular cylinders compressed in longitudinal direction. The sheets were rigidly built in at the sides parallel to the axis of the cylinder. |
| File Size | 7898085 |
| Page Count | 14 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930094536 |
| Archival Resource Key | ark:/13960/t5k96cs4m |
| Language | English |
| Publisher Date | 1938-01-01 |
| Access Restriction | Open |
| Subject Keyword | Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |