摘要
A power-matching methodology was promoted to decouple the interior-flow and external-flow of a tip-jet drive rotor, and a reaction drive model based on the engine exhaust gas property and duct flow condition was established, which including: influence of area, temperature, friction and rotor rotation. The rotor tension and torque was analyzed by a modified blade element method. The result shows that section thickness and rotary speed are main influential factors to the tension and power balance, and the represented method is a rapid approach to choose the jet rotor parameters in overall design stage.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 1787-1793 |
| 页数 | 7 |
| 期刊 | Hangkong Dongli Xuebao/Journal of Aerospace Power |
| 卷 | 26 |
| 期 | 8 |
| 出版状态 | 已出版 - 8月 2011 |
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