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Compressive-strength comparisons of panels having aluminum-alloy sheet and stiffeners with panels having magnesium-alloy sheet and aluminum alloy stiffeners
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1947 |
| File Size | 18878267 |
| Page Count | 41 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930081883 |
| Archival Resource Key | ark:/13960/t23c0cp7z |
| Language | English |
| Publisher Date | 1947-01-01 |
| Access Restriction | Open |
| Subject Keyword | Stressed Skin - Wings Metals - Magnesium Alloys, Sheet - Strength Metals - Downmetal Fs-1h Aluminum Alloys, Sheet - Alcoa 24st - Strength, Compressive Stiffners, Aluminum-alloy - Alcoa 24 St Z-shaped Stressed Skin-plates, Flat Stressed Skin - Stiffner Combinations - Buckling 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 |