An Eigen-Analysis of Rotary Wing Blades and Wake Coupled System with the Finite-State Inflow Model
學年 82
學期 1
發表日期 1993-12-06
作品名稱 An Eigen-Analysis of Rotary Wing Blades and Wake Coupled System with the Finite-State Inflow Model
作品名稱(其他語言) 旋翼尾流及葉片耦合之氣彈系統的特徵值分析
著者 王怡仁; Wang, Yi-Ren
作品所屬單位 淡江大學航空太空工程學系
出版者
會議名稱 太平洋國際航太科技會議=Pacific International Conference on Aerospace Science and Technology
會議地點 臺南, 臺灣
摘要 An eigenvalue study can provide stability information for a system, and it is also an important part of aeroelastic analysis. In this work, an eigen system of a three-dimensional unsteady wake model is studied first to understand the physical meaning of wake dynamics. The blade- wake coupled system eigen-analysis is studied by the Floquet Theory. The eigenvalues of the Floquet matrix can determine system characteristics. The effect of wake dynamics on rotor blade eigenvalues can be seen by comparison with no inflow case. The results show that the inflow has a profound effect on blade dynamics, even at high advance ratios.
關鍵字 特徵分析;旋轉翼葉片;尾流;有限狀態內流模式;氣彈性分析;前進比;穩定性;空氣動力阻尼;Eigen-Analysis;Rotary Wing Blade;Wake;Finite-State Inflow Model;Aeroelastic Analysis;Advance Ratio;Stability;Aerodynamic Damping
語言 en
收錄於
會議性質 國內
校內研討會地點
研討會時間 19931206~19931209
通訊作者 成功大學航空太空工程研究所; 行政院國家科學委員會; 教育部
國別 TWN
公開徵稿 Y
出版型式 紙本
出處 太平洋國際航太科技會議論文集(三)=Proceedings of Pacific International Conference on Aerospace Science and; Technology (Vol. III),頁1440-1446
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機構典藏連結 ( http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/18462 )

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