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Theory of helicopter damping in pitch or roll and a comparison with flight measurements
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1950 |
| File Size | 12480514 |
| Page Count | 28 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082758 |
| Archival Resource Key | ark:/13960/t04x9mw2t |
| Language | English |
| Publisher Date | 1950-10-01 |
| Access Restriction | Open |
| Subject Keyword | Damping IN Pitch Damping IN Roll Helicopters - Damping Helicopters - Stability Rotor Blades, Hinged 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 |