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A VORTEX MODEL OF A HELICOPTER ROTOR
A vortex model of a helicopter rotor is presented. Each blade of the rotor has three degrees of freedom: flapping, lagging and feathering. The motions after each degree of freedom are also known for all blades. The blade is modelled as a thin vortex surface. The wakes are free fluid surfaces. A syst...
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| 主要作者: | |
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| 格式: | Artigo |
| 語言: | Inglês |
| 出版: |
National Institute for Aerospace Research “Elie Carafoli” - INCAS
2009-06-01
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| 叢編: | INCAS Bulletin |
| 在線閱讀: | http://bulletin.incas.ro/files/valentin_butoescu_v1no1_full.pdf |
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