The Effect of Enthalpy Change on the Spray Behavior of Liquid Jet Laterally Injected into Supersonic Air Flow
碩士 === 國立成功大學 === 航空太空工程學系 === 103 === Combustion flow control is one of the key technologies in the development of supersonic combustion ramjet engine (Scramjet). The objective this thesis is to investigate the effects of temperature and pressure changes on liquid spray behavior in supersonic flow...
Main Authors: | Hung-BineHwang, 黃泓賓 |
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Other Authors: | Tony Yuan |
Format: | Others |
Language: | zh-TW |
Published: |
2015
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Online Access: | http://ndltd.ncl.edu.tw/handle/90973748848078318871 |
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