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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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Bibliographic Details
Main Authors: Zohary, Aideal Czar, Asrar, Waqar, Mohammed Aldheeb, Mohammed Abdulmalek
Format: Article
Language:English
English
Published: ISSR 2021
Subjects:
TL500 Aeronautics
Online Access: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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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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