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Numerical investigation on the pressure drag of some low-speed airfoils for UAV application

Progressive advancements in small to medium-sized fixed-wing UAVs call for prototype designing to be fast, accurate, and economical. This requires the numerical assessment of airfoil performance to be based on high fidelity replication of wind tunnel data. Furthermore, integration of drag reducti...

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Main Authors: Zohary, Aideal Czar, Asrar, Waqar, Mohammed Aldheeb, Mohammed Abdulmalek
格式: Article
語言:English
English
出版: ISSR 2021
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在線閱讀:http://irep.iium.edu.my/89039/7/89309_Numerical%20investigation%20on%20the%20pressure%20drag%20of%20some%20low-speed%20airfoils%20for%20UAV%20application_SCOPUS.pdf
http://irep.iium.edu.my/89039/13/89309_Numerical%20investigation%20on%20the%20pressure%20drag%20of%20some%20low-speed%20airfoils%20for%20UAV%20application.pdf
http://irep.iium.edu.my/89039/
http://akademiabaru.com/submit/index.php/cfdl/article/view/3075/2660
https://doi.org/10.37934/cfdl.13.2.2948
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