首页 | 本学科首页   官方微博 | 高级检索  
     检索      

用螺桨-吊舱相关法设计和分析桨扇
引用本文:朱年国,陈矛章,刘导治.用螺桨-吊舱相关法设计和分析桨扇[J].航空动力学报,1988,3(3):231-234,282.
作者姓名:朱年国  陈矛章  刘导治
作者单位:北京航空航天大学 (朱年国,陈矛章),北京航空航天大学(刘导治)
摘    要:本文用螺桨-吊舱相关分析法对桨扇进行设计和分析。用曲线升力线代表桨叶,并且考虑吊舱存在的影响;方法采用尾迹位于流面上的假定。对叶尖段进行跨音修正,对根部应用叶栅最佳损失攻角加以考虑。设计和分析的结果与文献〔2〕的计算和试验结果作部分比较,证明了本法的合理性和有效性,可以应用于桨扇的初步设计和性能分析中。

收稿时间:1987/12/1 0:00:00

PROPFAN DESIGN BY PRORELLER-NACELLE INTERACTION ANALYSIS
Zhu Nianguo,Chen Maozhang and Niu Daozhi.PROPFAN DESIGN BY PRORELLER-NACELLE INTERACTION ANALYSIS[J].Journal of Aerospace Power,1988,3(3):231-234,282.
Authors:Zhu Nianguo  Chen Maozhang and Niu Daozhi
Institution:Beijing Institute of Aeronautics and Astronautics;Beijing Institute of Aeronautics and Astronautics;Beijing Institute of Aeronautics and Astronautics
Abstract:A propeller-nacelle interaction analysis has been developed in this paper as a kind of lifting line analysis. It represents the blades by curved lifting lines, taking into Consideration the blade sweep and the effect of the nacelle on the propfan flowfield. The wake model assumes that the vortex filaments occur along stream surfaces. Some corrections have been made to transonic portion of the blade and large solidity cascade portion at hub. Comparison of the results of the design and analysis with those given in references show the method is feasible and effective, Aspects of its improvement are also discussed.
Keywords:
本文献已被 CNKI 等数据库收录!
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号