Study of Flow Field and Efficiency of Axial Flow Compressor
碩士 === 國防大學理工學院 === 機械工程碩士班 === 106 === The high-thrust-to-weight ratio aircraft engine needs a high performance compressor. The axial flow compressor is able to offer more mass flow rate and reach higher pressure ratio by employing multi-stage compression i.e. series combinations. Therefore, axial...
Main Authors: | LI, JIA-SHENG, 李佳生 |
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Other Authors: | TAI,CHANG-SHENG |
Format: | Others |
Language: | zh-TW |
Published: |
2018
|
Online Access: | http://ndltd.ncl.edu.tw/handle/y7vj93 |
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