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 reduction...

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Main Authors: Asrar, Waqar, Aldheeb, Mohammad, Zohary, Aideal Czar
格式: Article
语言:English
English
出版: Akademia Baru Publishing (M) Sdn Bhd 2021
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在线阅读:http://irep.iium.edu.my/88730/7/88730_Numerical%20investigation%20on%20the%20pressure%20drag%20of%20some%20low-speed%20airfoils%20for%20UAV%20application.pdf
http://irep.iium.edu.my/88730/13/88730_Numerical%20investigation%20on%20the%20pressure%20drag_SCOPUS.pdf
http://irep.iium.edu.my/88730/
http://www.akademiabaru.com/submit/index.php/cfdl/article/view/1080
https://doi.org/10.37934/cfdl.13.2.1228
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