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Fuselage stress analysis
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1920 |
| Description | Report analyzes the stresses in a fuselage of the built-up type in which the shear is taken by diagonal bracing wires. Tests are conducted for landing, flying, and thrust loads. |
| File Size | 1076607 |
| Page Count | 16 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930091137 |
| Archival Resource Key | ark:/13960/t46q54k7j |
| Language | English |
| Publisher Date | 1920-01-01 |
| 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 |