具扭角之葉片旋翼系統平衡後的空氣動力分析

機構典藏 > College of Engineering > Graduate Institute & Department of Aerospace Engineering > Journal Article > Item 987654321/46449

Please use this identifier to cite or link to this item: https://tkuir.lib.tku.edu.tw/dspace/handle/987654321/46449

Title:	具扭角之葉片旋翼系統平衡後的空氣動力分析
Other Titles:	An Aerodynamic Analysis of a Trimmed Twisted Rotor Blade System
Authors:	王怡仁;Wang, Yi-ren;唐鵬駿;Tang, P. J.;張立;Chang, L.
Contributors:	淡江大學航空太空工程學系
Keywords:	尾流動力學;具扭角之葉片;平衡Wake dynamics;Twisted blade;Trim
Date:	1997-09
Issue Date:	2013-03-20 16:24:22 (UTC+8)
Publisher:	臺南市：中國航空太空學會
Abstract:	本文利用升力線法和葉片元素理論模擬具扭角的旋翼葉片的空氣動力特性並和動力尾流理論相耦合而模擬旋翼之非穩態空氣動力環境。此外，本文利用自動操控的調適平衡法(auto pilot trim approach)取得葉片在此一振動系統下之升力及扭角在整個旋翼圓盤的最終穩態平衡值；本文所考慮的系統是一尾流、升力、及葉片外形扭角三者相互影響的閉迴路系統，其中任一項的改變都會導致其他二者的改變。本系統所發展的模式可成功預測旋翼在不同的飛行姿態且達到平衡時旋翼圓盤的升力及攻角分佈。 In this work, the lifting line method and blade element theory are used to formulate a twisted rotor blade lift distribution and coupled with dynamic wake model to simulate the unsteady aerodynamic environment of a lifting rotor. The auto pilot trim approach is applied to the rotor system subject to a lift equilibrium condition in such a wake vibrating system. Results show that our model successfully predicts the lift and angle of attack distribution on the trimmed rotor disk.
Relation:	中國航空太空學會學刊=Transactions of the Aeronautical and Astronautical Society of the Republic of China 29(3)，頁217-226
Appears in Collections:	[Graduate Institute & Department of Aerospace Engineering] Journal Article

Files in This Item:

File	Size	Format
index.html	0Kb	HTML	218	View/Open

Loading...