Study on Combustor Component Test and Diagnostics of a Micro Turbojet Engine
碩士 === 國立成功大學 === 航空太空工程學系 === 86 === The combustor is an important component in turbojet engines. Gas turbinecombustor needs to be designed to meet many design requirements, includinghigh combustion efficiency over a wide operating envelop, stable operat...
| Main Authors: | , |
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| Format: | Others |
| Language: | zh-TW |
| Published: |
1998
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| Online Access: | http://ndltd.ncl.edu.tw/handle/97756838275258119851 |