Low Reynolds Number High- Lift Airfoil Design for HALE Concept UAV

机译：适用于HALE概念无人机的低雷诺数高升翼型设计

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来源
《24th Applied Aerodynamics Conference》|2006年|P.1-18|共18页
会议地点 San Francisco CA(US)
作者
Q. Liu; J. Li; Z. Zhou;
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作者单位

School of Aeronautics, Northwestern Polytechnical University, Xi'an, China (prc);

School of Aeronautics, Northwestern Polytechnical University, Xi'an, China (prc);

UAV Research and Development Center, Northwestern Polytechnical University, Xi'an, China (prc);

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中图分类空气动力学;
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4. Low Reynolds Number High- Lift Airfoil Design for HALE Concept UAV [C] . Applied Aerodynamics Conference . 2006

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Low Reynolds Number High- Lift Airfoil Design for HALE Concept UAV

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