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: | |
| 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 |