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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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| Format: | Artigo |
| Sprache: | Inglês |
| Veröffentlicht: |
National Institute for Aerospace Research “Elie Carafoli” - INCAS
2009-06-01
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| Schriftenreihe: | INCAS Bulletin |
| Online Zugang: | http://bulletin.incas.ro/files/valentin_butoescu_v1no1_full.pdf |
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