WB：翼身

“Wing Body”一词在工程与交通运输领域常被简写为“WB”，以提升书面及口头表达的效率。其核心含义为“翼身”，通常用于描述飞行器或高速运载工具中机身与机翼一体化的结构设计。这种缩写形式在技术文档、行业报告及日常交流中应用广泛，便于专业人员快速识别和引用。

In this paper, the bonding technique for the blended wing body mini UAV is presented.
本文介绍了翼身(WB)融合体无人机的胶接技术。
A new type of transport, which is different from the conventional cylinder fuselage plus wing but a blended wing body ( BWB ), is discussed.
讨论了一种区别于机翼与圆柱机身的传统民机外形&翼身(WB)融合体（BWB）外形。
Both simulation and experimental results can reflect accurately the strain variation of the wing body structure under the coupled action of the stress and temperature fields.
仿真研究与实验测试结果均能够准确反映翼体结构在应力场与温度场耦合作用下翼体翼表结构的应变变化情况。
A prime project of a blended wing body vehicle with canard is provided, and through the change of the fuselage head form and the different fin disposals, the RCS are optimized.
对初步形成的鸭翼-翼身(WB)融合体改变机身头部形状和立尾配置等进行RCS优化。
Research of grid spacing and orthogonality control in three dimensional flows around a wing body tail combination
网格间距及正交性控制在翼-身-尾组合体三维绕流中的研究

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