Design and Numerical Study on Aerodynamics Performance for F16 Leading Edge Extension
碩士 === 國立成功大學 === 航空太空工程學系 === 106 === In this research, we use commercial software, ANSYS CFX, to carry out the simulations of the F16 aerodynamics flow fields. The flight with a modified Leading Edge Extension (LEX) is proposed to increase the lift/drag ratio. The Shear Stress Transport k-ω turbul...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2018
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| Online Access: | http://ndltd.ncl.edu.tw/handle/r53785 |