Study of Steady Mode Dielectric Barrier Discharge Plasma Actuators on a Delta Wing
碩士 === 國立成功大學 === 航空太空工程學系 === 102 === The aim of this study is to investigate the aerodynamic performance of a delta wing using the airflow control method. The wind tunnel experiment is used to obtain the aerodynamic characteristics as a surface plasma actuator, set on the leading edge of a delta w...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2014
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| Online Access: | http://ndltd.ncl.edu.tw/handle/54747850457627309426 |