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Total main rotor isolation system analysis (Document No: 19810011499)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Sankewitsch, V. |
| Copyright Year | 1981 |
| Description | Requirements, preliminary design, and verification procedures for a total main rotor isolation system at n/rev are presented. The fuselage is isolated from the vibration inducing main rotor at one frequency in all degrees of freedom by four antiresonant isolation units. Effects of parametric variations on isolation system performance are evaluated. |
| File Size | 1808596 |
| Page Count | 83 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810011499 |
| Archival Resource Key | ark:/13960/t0xq1tf6f |
| Language | English |
| Publisher Date | 1981-03-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Vibration Isolators Systems Engineering Structural Vibration Rotating Bodies Resonant Vibration Rotor Aerodynamics Product Development Fuselages Shock Absorbers Aircraft Structures Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |