翼身融合体：一般的飞机是由机翼与机身两个部件接合而成的，在机翼与机身的交接处， 机身的侧面与机翼表面构成直角（或接近于直角），这样的组合，由于浸润面积大，阻力也较大。
本文介绍了翼身融合体无人机的胶接技术。
In this paper, the bonding technique for the blended wing body mini UAV is presented.
从全速位方程出发研究了机翼和翼身融合体跨音速绕流的有限元算法。
The finite element algorithm for transonic flows about wing and blended wing-body configuration is investigated based on the full potential equations.
讨论了一种区别于机翼与圆柱机身的传统民机外形——翼身融合体(BWB)外形。
A new type of transport, which is different from the conventional cylinder fuselage plus wing but a blended wing body (BWB), is discussed.
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