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: | , , |
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| Format: | Article |
| Language: | English English |
| Published: |
ISSR
2021
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| Subjects: | |
| 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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