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...
Main Authors: | , |
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Other Authors: | |
Format: | Others |
Language: | zh-TW |
Published: |
1998
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Online Access: | http://ndltd.ncl.edu.tw/handle/60958328443429850828 |