Propeller locations study on delta-winged unmanned aerial vehicle (UAV) model
Delta wing design is being used in aircraft to obtain high manoeuvre properties. The flow above the delta wing is complicated and dominated by a very complex vortex structure. This research investigates the effects of the propeller locations on the aerodynamic characteristics above a generic 55° sha...
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| 主要作者: | |
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| 格式: | Thesis |
| 語言: | English |
| 出版: |
2017
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| 主題: | |
| 在線閱讀: | http://eprints.utm.my/id/eprint/78655/1/KhushairiAmriKasimMFKM2017.pdf |
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