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Tests of 10-inch 24s-t aluminum-alloy shear panels with 1-1/2-inch holes i
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1943 |
| File Size | 6399865 |
| Page Count | 14 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930093375 |
| Archival Resource Key | ark:/13960/t7pp29s2k |
| Language | English |
| Publisher Date | 1943-01-01 |
| Access Restriction | Open |
| Subject Keyword | Effect OF Holes Diagrams, Stress-strain Aluminum Alloys, Sheet-alcoa 24st-strength 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 |