A Hybrid method for Helicopter Rotor Blade Optimum Design

碩士 === 淡江大學 === 航空太空工程學系 === 86 === This study presents an application of hybrid method for a helicopter rotor blade design through an unsteady aerodynamic consideration. Two strategies will be discussed and compared which is start...

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Bibliographic Details
Main Authors: Lin, Chyi-Feng, 林奇鋒
Other Authors: Chang Yeong-Kang
Format: Others
Language:zh-TW
Published: 1998
Online Access:http://ndltd.ncl.edu.tw/handle/71306803391932275675