Numerical study on joined : wing aircraft
A joined wing aircraft model B150 and conventional aircraft model D150 was selected to be examined. Fluent was used to conduct Reynolds-Averaged Naiver-Stokes simulation on the aerodynamic characteristics, such as lift and drag under varied angle of attack, under transonic speed. The lift and drag c...
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| 格式: | Final Year Project |
| 語言: | English |
| 出版: |
Nanyang Technological University
2020
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| 主題: | |
| 在線閱讀: | https://hdl.handle.net/10356/145590 |
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