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A numerical method for studing the transient blade motions of a rotor with flapping and lead-lag degrees of freedom
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1967 |
| Description | Numerical method for determining transient blade motions of rotor with flapping and lead-lag degrees of freedom |
| File Size | 1212513 |
| Page Count | 36 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19670028687 |
| Archival Resource Key | ark:/13960/t5t774x7t |
| Language | English |
| Publisher Date | 1967-10-01 |
| Access Restriction | Open |
| Subject Keyword | Transient Response Rotor Blade Dynamic Stability Motion Equation Numerical Analysis Helicopter Rotor 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 |