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...

Full description

Saved in:
Bibliographic Details
Main Authors: Asrar, Waqar, Aldheeb, Mohammad, Zohary, Aideal Czar
Format: Article
Language:English
English
Published: Akademia Baru Publishing (M) Sdn Bhd 2021
Subjects:
Online Access: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
Tags: Add Tag
No Tags, Be the first to tag this record!
Institution: Universiti Islam Antarabangsa Malaysia
Language: English
English