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...

وصف كامل

محفوظ في:
التفاصيل البيبلوغرافية
المؤلفون الرئيسيون: Zohary, Aideal Czar, Asrar, Waqar, Mohammed Aldheeb, Mohammed Abdulmalek
التنسيق: مقال
اللغة:English
English
منشور في: ISSR 2021
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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