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Formulas for the stress analysis of circular rings in a monocoque fuselage
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1933 |
| Description | The formulas given in this report provide a simplified method for the stress-analysis of fuselage bulkheads that are approximately circular rings of uniform cross section. Complicated load systems acting on a ring can usually be resolved into simplified load systems; and formulas for moment, axial force, and shear for such simplified load systems are given in this report. Illustrative examples showing the use of this method in practical stress-analysis work are also included. |
| File Size | 14573030 |
| Page Count | 30 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930081328 |
| Archival Resource Key | ark:/13960/t9089fz2b |
| Language | English |
| Publisher Date | 1933-01-01 |
| 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 |