The Analysis of Aerodynamic Performance on the Flapping Wings
碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 93 === A numerical method is developed to study the flapping wing flowfields. The method uses finite-volume method to solve the Euler equation. A diagonal dominant alternating direction implicit scheme (DDADI) coupling with an implicit residual smoothing is used...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2005
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| Online Access: | http://ndltd.ncl.edu.tw/handle/91176404150986268419 |