Based on the aerofoil NACA0030,some aerodynamic configurations of row flying-wings with the higher volume efficiency(volume /surface) were constructed. Different arrayed row flying-wings were calculated and investigated minutely.
以NACA0030翼型为基础,构造了具有较高体积率(体积/表面积)的排式飞翼气动布局。
参考来源 - 一种新型浮升一体化排式飞翼的设计与研究·2,447,543篇论文数据，部分数据来源于NoteExpress
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