Aerodynamics of a Modified High-Lift Low Reynolds Number Airfoil: Preliminary Analysis
Airfoil selection is a crucial phase in the design of a small unmanned fixed-wing aircraft to allow a minimum size and weight of the lifting surfaces. The present study analyzesairfoils to be used in low operating Reynolds number unmanned aerial vehicles (UAV) using XFLR5 software, which was validat...
الحاوية / القاعدة: | International Journal of Emerging Technology and Advanced Engineering |
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المؤلف الرئيسي: | Hamid A.H.A.; Mohamad F.; Noh M.H.M.; Nasir R.E.M.; Sapardi M.A.M. |
التنسيق: | مقال |
اللغة: | English |
منشور في: |
IJETAE Publication House
2022
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الوصول للمادة أونلاين: | https://www.scopus.com/inward/record.uri?eid=2-s2.0-85145034334&doi=10.46338%2fijetae1222_02&partnerID=40&md5=6b108eaf47cf6e862a4bb20084bdcb88 |
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