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Compressive strength of 24s-t aluminum-alloy flat panels with longitudinal formed hat-section stiffeners having a ratio of stiffener thickness to skin thickness equal to 1.00
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1947 |
| File Size | 9663806 |
| Page Count | 23 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082069 |
| Archival Resource Key | ark:/13960/t4fn5hb21 |
| Language | English |
| Publisher Date | 1947-01-01 |
| Access Restriction | Open |
| Subject Keyword | Stressed Skin-stiffener Combinations - Strength, Compressive Charts - Stressed Skin Stressed Skin-stiffener Combinations - Buckling Aluminum Alloys, Sheet - Alcoa 24st - Strength, Compressive Stiffeners, Aluminum-alloy - Alcoa 24st Hat-shaped 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 |