Active control of helicopter vibration
โ Scribed by Pearson, J.T.; Goodall, R.M.; Lyndon, I.
- Book ID
- 114440958
- Publisher
- The Institution of Electrical Engineers
- Year
- 1994
- Tongue
- English
- Weight
- 915 KB
- Volume
- 5
- Category
- Article
- ISSN
- 0956-3385
No coin nor oath required. For personal study only.
๐ SIMILAR VOLUMES
The compensation of wbraUons generated by the rotor of a helicopter and transmitted to the cabin is of great importance for rotorcraft design These vlbraUons occur at discrete, well known frequencies, the so-called rotor-blade harmomc frequencies In this paper the apphcatlon of actwe control technol
The active control of flow-induced oscillations, specifically, vortex-induced oscillations of circular cylinders and galloping oscillations of circular cylinders and galloping oscillations of a square prism, are considered. In the case of vortex-induced oscillations, the vibrating cylinder is modele