摘要
An improved aerodynamics model for cycloidal propellers based on Leishman-Beddoes(LB) dynamical stall model is presented in this paper. The validations are made between the experimental data and the results from presented model. The validations proved that the presented model is applicable for cycloidal propeller performance evaluation under hovering status. Based on the analysis with the calculation results, some of the mechanisms about how the efficiency of cycloidal propeller could be improved are revealed.
| 源语言 | 英语 |
|---|---|
| 页 | 1413-1417 |
| 页数 | 5 |
| 出版状态 | 已出版 - 2012 |
| 活动 | 28th Congress of the International Council of the Aeronautical Sciences 2012, ICAS 2012 - Brisbane, 澳大利亚 期限: 23 9月 2012 → 28 9月 2012 |
会议
| 会议 | 28th Congress of the International Council of the Aeronautical Sciences 2012, ICAS 2012 |
|---|---|
| 国家/地区 | 澳大利亚 |
| 市 | Brisbane |
| 时期 | 23/09/12 → 28/09/12 |