| 螺旋桨升力线理论的匹配渐近展开法分析 |
| |
| 引用本文： | 陈泽民,潘杰元,吴礼义.螺旋桨升力线理论的匹配渐近展开法分析[J].航空学报,1994,15(5):513-518. |
| |
| 作者姓名： | 陈泽民 潘杰元 吴礼义 |
| |
| 作者单位： | 北京航空航天大学流体力学研究所,北京,100083 |
| |
| 摘 要： | 在固连于螺旋桨桨叶的非惯性坐标系中,对大展弦比叶片的螺旋奖建立了升力线模型。在匹配渐近展开法分析中引入一假想速度位,导出固连坐标系中的控制方程、边界条件和Ｂｅｒｎｏｕｌｌｉ方程。由匹配渐近展开法的分析表明,在螺旋桨的进距比不是太小的情况下,螺旋桨的升力线理论在固连于螺旋桨桨叶的非惯性坐标系中仍然成立。
|
| 关 键 词： | 螺旋桨 匹配 渐近法 |
| 收稿时间： | 1993-01-14 |
| 修稿时间： | 1993-09-10 |
IHE ANALYSIS OF PROPELLELLER LIFTING LINE THEORY BY THE METHOD OF MATCHED ASYMPTOTIC EXPANSIONS |
| |
| Chenzemin,Pan Jieyuan,Wu Liyi.IHE ANALYSIS OF PROPELLELLER LIFTING LINE THEORY BY THE METHOD OF MATCHED ASYMPTOTIC EXPANSIONS[J].Acta Aeronautica et Astronautica Sinica,1994,15(5):513-518. |
| |
| Authors: | Chenzemin Pan Jieyuan Wu Liyi |
| |
| Institution: | Institute of Fluid Mechanics,Beijing University of Aeronautics and Astronautics,Beijing,100083 |
| |
| Abstract: | Lifting line model has been developed for propeller of large aspect ra tio in blade-at-tached noninertial system,In the analysis of the method of matched asymptotic expansions,ficti-tious velocity potential is introduced.Control equation, boundary condition and Bernoulli equation are derived in blade-attached system. The analysis of the matched asymptotic expansions shows that if the advaneed ratio of propeller is not very small,lifting line theory itq still valid in blade-at-tached noninertial system for propeller. |
| |
| Keywords: | propellers matching asymptotic methods |
| 本文献已被 CNKI 等数据库收录！ |
| 点击此处可从《航空学报》浏览原始摘要信息 |
| 点击此处可从《航空学报》下载免费的PDF全文 |
|
