Optimum Design on Wing Frame of Low Reynolds number Micro-Aerial-Vehicle based on CFD Data
碩士 === 國防大學理工學院 === 機械工程碩士班 === 97 === There flight efficiency, stability and control model of micro-aerial-vehicles （MAVs）during cruise all are strongly dependent on the wings’ aerodynamic performance. Unlike the traditional transport vehicles, the flow condition of MAV is belonging to the low Reyn...
| Main Authors: | , |
|---|---|
| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2009
|
| Online Access: | http://ndltd.ncl.edu.tw/handle/42645272563653898085 |