摘要
The introduction of the full paper discusses relevant matters and then proposes the analysis mentioned in the title. Sections 1 through 3 explain our analysis of the drag characteristics. We believe that all the results of our analysis can serve as effective guidelines for configuration design of lift-fan VTOL. Their core consists of: (1) we establish the aerodynamic estimation model of the lift-fan VTOL; (2) we analyze the effects of conceptual parameters on the peak drag of the lift-fan VTOL in its transition mode. Section 4 presents five conclusions for the results shown in Figs. 2 through 10 in section 3 and three effective guidelines for the configuration design of lift-fan VTOL.
| 源语言 | 英语 |
|---|---|
| 页（从-至） | 6-10 |
| 页数 | 5 |
| 期刊 | Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University |
| 卷 | 30 |
| 期 | 1 |
| 出版状态 | 已出版 - 2月 2012 |