Aerodynamic Analysis of Low Reynolds Number Thin Airfoil for MAV
碩士 === 國防大學中正理工學院 === 兵器系統工程研究所 === 96 === The aerodynamic characteristics of four types of low Reynolds number airfoils at Re=5.0x10^4 and Re=1.6x10^5 were systematically simulated in present work. The tested airfoil models included of NACA0003, NACA0012, NACA 5403, and NACA6403 with aspect ratio r...
| Main Authors: | , |
|---|---|
| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2008
|
| Online Access: | http://ndltd.ncl.edu.tw/handle/27745708748626673370 |