Loading...
Please wait, while we are loading the content...
Similar Documents
Ultimate stresses developed by 24s-t sheet in incomplete diagonal tension
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1941 |
| Description | Tests were made on 18 shear panels of 24S-T aluminum alloy to verify the dependence of the ultimate stress on the degree of development of the diagonal-tension field. Tests were made on two thicknesses of sheet with the sheet either clamped between the flange angle or riveted to the outside of the angles. |
| File Size | 6868741 |
| Page Count | 12 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930081574 |
| Archival Resource Key | ark:/13960/t5t75m59z |
| Language | English |
| Publisher Date | 1941-01-01 |
| 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 |