直升机新型旋翼翼型气动特性与布局分析

V211.52; 利用结构网格计算流体力学(Computational fluid dynamics,CFD)的翼型气动特性分析方法开展旋翼翼型气动特性计算.通过RAE282,NACA0012,OA212,OA207等翼型压力分布、升力和阻力等特性计算结果与试验结果的对比分析,验证了计算方法的准确性,并进一步完成了HF系列旋翼翼型的气动特性计算.基于翼型的气动特性,采用时间步进自由尾迹的旋翼气动性能分析方法开展旋翼桨叶翼型的气动布局优化设计,对悬停和前飞条件下的旋翼开展计算分析,得到两种条件下的旋翼气动特性.而后通过本文建立的优化方法开展旋翼翼型布局优化设计....

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Published in南京航空航天大学学报 Vol. 52; no. 2; pp. 318 - 333
Main Authors 李生伟, 熊俊卿, 王鑫磊
Format Journal Article
LanguageChinese
Published 哈尔滨哈飞航空工业有限责任公司飞机设计所,哈尔滨,150066%陆军装备部航空军事代表局,北京,100000 01.04.2020
Subjects
翼型
自由尾迹
旋翼
布局分析
气动特性
Online AccessGet full text
ISSN1005-2615
DOI10.16356/j.1005-2615.2020.02.019

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Abstract V211.52; 利用结构网格计算流体力学(Computational fluid dynamics,CFD)的翼型气动特性分析方法开展旋翼翼型气动特性计算.通过RAE282,NACA0012,OA212,OA207等翼型压力分布、升力和阻力等特性计算结果与试验结果的对比分析,验证了计算方法的准确性,并进一步完成了HF系列旋翼翼型的气动特性计算.基于翼型的气动特性,采用时间步进自由尾迹的旋翼气动性能分析方法开展旋翼桨叶翼型的气动布局优化设计,对悬停和前飞条件下的旋翼开展计算分析,得到两种条件下的旋翼气动特性.而后通过本文建立的优化方法开展旋翼翼型布局优化设计.
AbstractList V211.52; 利用结构网格计算流体力学(Computational fluid dynamics,CFD)的翼型气动特性分析方法开展旋翼翼型气动特性计算.通过RAE282,NACA0012,OA212,OA207等翼型压力分布、升力和阻力等特性计算结果与试验结果的对比分析,验证了计算方法的准确性,并进一步完成了HF系列旋翼翼型的气动特性计算.基于翼型的气动特性,采用时间步进自由尾迹的旋翼气动性能分析方法开展旋翼桨叶翼型的气动布局优化设计,对悬停和前飞条件下的旋翼开展计算分析,得到两种条件下的旋翼气动特性.而后通过本文建立的优化方法开展旋翼翼型布局优化设计.
Author 李生伟
王鑫磊
熊俊卿
AuthorAffiliation 哈尔滨哈飞航空工业有限责任公司飞机设计所,哈尔滨,150066%陆军装备部航空军事代表局,北京,100000
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Author_FL LI Shengwei
WANG Xinlei
XIONG Junqing
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自由尾迹
旋翼
布局分析
气动特性
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Title 直升机新型旋翼翼型气动特性与布局分析
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