COMPUTATIONAL FLUID DYNAMICS BASED WINGLET DESIGN AND ANALYSIS OF GL-1 GLIDER
Winglet is the most effective device installed in wing tip to reduce induced drag which is the second largest contribution of drag especially in a low-speed aircraft. The drag is from wingtip vortex. In the previous study, GL-1 have not added yet by winglet and the aerodynamic efficiency was 27 o...
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| 格式: | Final Project |
| 語言: | Indonesia |
| 在線閱讀: | https://digilib.itb.ac.id/gdl/view/41567 |
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