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...
Saved in:
Main Authors: | , , |
---|---|
格式: | Article |
語言: | English English |
出版: |
Akademia Baru Publishing (M) Sdn Bhd
2021
|
主題: | |
在線閱讀: | 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 |
標簽: |
添加標簽
沒有標簽, 成為第一個標記此記錄!
|
成為第一個發表評論!