Oscillation Characteristics of Shock Waves in a Transonic Nozzle

博士 === 國立成功大學 === 航空太空工程學系 === 86 === The self-excited oscillations of shock wave in transonic channel flow havebeenexperimentally investigated in an especially designed, constructedand tested high speed jet facility. Two types of flow visualizationtechni...

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Bibliographic Details
Main Authors: Wang, Bih-Chang, 王必昌
Other Authors: Fan-Ming Yu
Format: Others
Language:zh-TW
Published: 1998
Online Access:http://ndltd.ncl.edu.tw/handle/60958328443429850828