ロード中...
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...
保存先:
| 第一著者: | |
|---|---|
| フォーマット: | Artigo |
| 言語: | Inglês |
| 出版事項: |
National Institute for Aerospace Research “Elie Carafoli” - INCAS
2009-06-01
|
| シリーズ: | INCAS Bulletin |
| オンライン･アクセス: | http://bulletin.incas.ro/files/valentin_butoescu_v1no1_full.pdf |
| タグ: |
タグ追加
タグなし, このレコードへの初めてのタグを付けませんか!
|