The Experiment of SDOF Transonic Cascade Flutter Suppression - Construction of the Active Acoustic Control Facilities
碩士 === 國立成功大學 === 航空太空工程學系 === 88 === Flutter analysis is a required step that has to be validated in the design loop of a new engine. Active acoustic control technique is a potential candidate that could be considered for suppressing engine blade flutter. Acoustic flutter control calls...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2000
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| Online Access: | http://ndltd.ncl.edu.tw/handle/96607107588269794092 |