Abstract
In the paper, Based on the low Reynolds number aerodynamics of the micro air vehicles (MAVs), some researches were done, such as aerodynamics characteristic numerical analysis research on the airfoil at low Reynolds numbers, numerical calculation method of low Mach low Reynolds numbers fluid field, estimation method research on aerodynamic characteristic of the aeroelastic flapping wing, unsteady vortex method of aerodynamics characteristic estimation and wind tunnel test of MAVs. The results of this paper have important reference value and instructive meaning to the development of MAVs.
Original language | English |
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Pages (from-to) | 137-141 |
Number of pages | 5 |
Journal | Xitong Gongcheng Lilun yu Shijian/System Engineering Theory and Practice |
Volume | 25 |
Issue number | 9 |
State | Published - Sep 2005 |
Keywords
- Flapping wing
- Micro air vehicles (MAVs)
- Reynolds number
- Wind tunnel test