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...
محفوظ في:
المؤلفون الرئيسيون: | , , |
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التنسيق: | مقال |
اللغة: | English English |
منشور في: |
ISSR
2021
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الموضوعات: | |
الوصول للمادة أونلاين: | 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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