The leading contender is the fabled blended-wing body, which replaces the conventional tube with a triangular shape.
先进的混合机翼体，用三角造型代替了传统的管型。
In this paper, the bonding technique for the blended wing body mini UAV is presented.
本文介绍了翼身融合体无人机的胶接技术。
The experimental studies on two wing body junctions and wakes were carried out in a low turbulence level wind tunnel.
绕两个翼型-平面的角区流动及其尾迹的实验是在低湍流度风洞中完成的。
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——翼身融合体(BWB)外形。
NASA's Glenn Research Center dedicated a model of the hybrid wing body, a futuristic aircraft concept, on July 8, 2009.
美国航空航天局格伦研究中心展出了混合型飞行器模型——下一代未来飞行器的概念模型。
Numerical results show that present method is an effective one for solving the flow around wing body configuration with control surface deflection.
数值算例表明本文方法是求解带操纵面偏转的翼身组合体绕流的有效方法。
Numerical results show that the present method is effective one for solving the flow around a wing body combination with control surface deflection.
数值算例表明该方法是求解带操纵面偏转的翼身组合体绕流的有效方法。
Hybrid Wing Body H-Series future aircraft design concept comes from the research team led by the Massachusetts Institute of Technology.
翼身混合h系列未来飞机的设计概念是来自美国麻省理工学院领导的研究团队。
The Hybrid Wing Body H-Series future aircraft design concept comes from the research team led by the Massachusetts Institute of Technology.
上图所示的这款H系列的体翼混合未来飞行器设计构思来自由麻省理工学院的研究小组。
The viscous flow around M6 wing and F4 wing-body configuration are simulated and compared with the results of wind tunnel experiment.
为了验证方法和程序的正确性，论文中对M6机翼和F4翼身组合体的流场进行了数值模拟，并与试验结果进行了对比。
The flat body sides are aligned with the canted tails, the wing-body junction is clean, and there is a sharp chine line around the forward fuselage.
扁平的机身侧部与倾斜的垂尾处于同一面上，翼身衔接处光滑，前机身被一清晰的脊线环绕。
It is shown that only a few changes needed to expand the computer program for wing alone to cover wing-body combinations.
本文指出，只需少量修改，就可将单独翼分析程序扩展为可同时适用于翼-身组合体。
The finite element algorithm for transonic flows about wing and blended wing-body configuration is investigated based on the full potential equations.
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 research on aerodynamic characteristics of wrap-around fin and wing-body combination was carried out at super high speeds in this dissertation.
本文开展了弧形翼及翼-身组合体在超高速下的空气动力学特性研究。
The lifting-body shape of the wing-body combination has become the main design direction of the hypersonic vehicle due to its internal loading and lift-drag characteristics.
翼身组合的升力体外形由于兼顾内部装填以及升阻特性成为了目前高速飞行器主要的设计方向。
The saucer-shaped aircraft is a novel aircraft adopting blend-wing-body configuration.
碟形飞行器是一种新颖的，采用翼身融合布局的飞行器。
And the viscous separation flow of wing-body trailing edge conjunction can be effectively simulated. Therefore these algorithms are valuable for the engineering applications.
计算结果与风洞实验的对比表明，文中所采用的数值方法可以有效的模拟翼身结合处粘性分离流动，具有一定的工程实用价值。
Give a new description of blend - Wing - Body (BWB) blend tolerance. Model surface plane grid for calculating both aerodynamic force and stealth.
提出了融合度描述方法，通过建立统一的表面面元模型分析计算融合对气动特性和隐身特性的影响。
Give a new description of blend - Wing - Body (BWB) blend tolerance. Model surface plane grid for calculating both aerodynamic force and stealth.
提出了融合度描述方法，通过建立统一的表面面元模型分析计算融合对气动特性和隐身特性的影响。
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