Acoustic Forcing of Transonic Compressor Rotor with Viscous and Tip Clearance Effects

碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 95 === The purpose of the present study is to investigate the viscous and tip clearance effects on the transonic rotor 67 under acoustic excitations. A high-resolution aeroacoustic Navier-Stokes flow solver that can capture shock wave and resolve acoustic waves was...

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Bibliographic Details
Main Authors: Sin-You Wang, 王信祐
Other Authors: Pong-Jeu Lu
Format: Others
Language:zh-TW
Published: 2006
Online Access:http://ndltd.ncl.edu.tw/handle/87643123327171423444