We conceived the new Contemporary Art + Design Wing as a "building on the green" – a structure that operates both as an organizing element and is also emblematic of its contemporary contents.
我们构想了新的当代艺术+设计翼楼作为一栋“绿地上的建筑”—这栋建筑既是一个组织要素，也是其所展出的当代艺术品的一个象征。
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。
But at a glance, the efficient wing design and engines appear to be holding up their end of the deal.
粗看之下，更有效的机翼与发动机设计保证了公司有效的实现他们的目标。
The aerofoil of a wing creates more lift than drag, but exactly how much depends on its design and the speed of the air passing over it.
飞机上的机翼制造升力超过阻力，但具体取决于机翼的设计和当时经过的空气流动速率。
However, advances in rapid prototyping have greatly expanded the possibilities for wing design, allowing wing shapes to replicate those of real insects or virtually any other shape.
然而，快速成形技术的迅猛发展大大提高了翅翼设计的可能性，完全能够复制真实昆虫的翅翼形状，事实上可以刻画任何形状。
MIT’s D “double bubble” series design concept is based on a modified “tube-and-wing” structure that has a very wide fuselage to provide extra lift.
麻省学院的D型“两个泡泡”系列设计概念基于改进过的“管状机身和一对后倾机翼”结构，机身更加宽大，可以提供额外的升力。
611 institute (Chengdu Aircraft Design institute) initiated studied on the "tailless delta-canard" wing planform as early as the late 1960s.
611所(成都飞机设计院)早在1960年代末就开始研究鸭式无尾三角翼布局飞行平台。
A NATO working group has established common standards for the design and construction of fixed-wing unmanned aerial vehicles.
日前，一个北约(NATO)工作组建立了设计和建造固定翼无人机的通用标准。
With the right design, a uniform stream of light has pushed tiny objects in much the same way that an airplane wing hoists a 747 off the ground.
研究人员采用一合理设计，使用均匀的光束照射微小物体从而让它们像747客机一样离开地面飞了起来。
Composite wing design, in which involved are many disciplines such as structural mechanics, aerodynamics and control engineering, is a complicated process.
复合材料翼面设计是一个涉及结构力学、空气动力学和控制工程等多个学科的复杂过程。
Missile carrying on the wing tip causes the wing structure design and analysis to face many challenges, such as structural vibration response and aeroelastic response.
飞机机翼挂装翼尖导弹对机翼结构设计和结构分析提出了诸多全新课题，如结构的振动响应和气动弹性动响应。
Wing design, to bring professional design team and strategy think-tank, feel the trend of the market, lending industry design trend.
甲由设计，携专业设计团队和策略智囊，感受市场潮流趋势，引领工业设计风潮。
General Jan Dodonna conceived of the A-wing starfighter design after analyzing the role raw speed played in the Battle of Yavin, and researching the performance of Tammuz-an R-22 Spearhead fighters.
简·多登纳将军分析了原始速度在雅文战役中的作用，研究了塔穆兹-昂r - 22“矛头”战斗机后，构思了A翼星际战斗机的设计。
The simulation results provide theoretical basis for the design and optimization on the crafts of wing in ground effect .
研究结果为地效飞行器的设计与优化提供理论依据。
The latter are a clear reflection of the structural design, most clearly seen on the south wing facade which incorporates the shape of a three-meter high Vierendel carrier.
铝条清晰地反映出结构设计，这从南侧立面上有所体现，它包含了一个三米高的高华伦氏支架。
Then the gradients of flutter speed and frequency of wing with respect to the design variables were deduced with analytical method.
使用解析方式推导得到机翼的临界颤振速度、颤振频率对于设计变量的灵敏度表达式。
The study shows that developing knowledge-driven design tools should be a feasible approach to the wing structural layout problem.
研究表明，开发知识驱动的设计工具，是解决机翼结构布局设计问题的一条可行途径。
Combining dynamic design of wing flutter model for a giant transport aircraft, a numerical example of engineering application is presented.
结合某大型飞机机翼颤振吹风模型的动力设计，本文给出了工程应用的具体数值例子。
Research on the parameters which the spreading performance influence is of great significance to the design and the improvement of the folding wing.
折叠翼的展开性能参数是折叠翼设计的重要指标，研究它对于设计和改进折叠翼具有重要意义。
To test this algorithm, one design example, one rib of an aircraft wing, is given.
为验证该算法，给出了一个飞机水平安定面翼肋设计实例。
In the design of joined wing, the complex and the interaction between each specialities and subjects are unknown from previous design experience.
连翼布局飞机设计中，各专业学科之间的相互影响和复杂性是以前的设计中所未知的。
The aerodynamic computation and the design of optimized wing sails for aircraft with rectangular wing whose aspect ratio equals 8. 6 were completed.
以展弦比为8.6的机翼加装帆片为例，进行了气动力计算并作了帆片优化设计。
On the basis of the canard configuration a contour stealthy design including chiefly the wing, the fuselage and their connection type is projected.
在鸭式布局的基础上，对飞行器各部件及部件间的连接方式进行了外形隐身设计。
The effects of wing-fuselage fusion design parameter have been analyzed.
分析了翼身融合设计参数的影响。
The computational results show that there is an important significance in the optimum design of wing configurations of aerospace vehicle.
计算结果表明，航天飞机机翼外形优化设计具有重要意义。
The main problems include general design of towed system, controllable wing design and intergration of optical sensors.
着重解决的问题包括拖曳系统的总体设计、控制翼的设计以及光学类传感器的集成。
The main problems include general design of towed system, controllable wing design and intergration of optical sensors.
着重解决的问题包括拖曳系统的总体设计、控制翼的设计以及光学类传感器的集成。
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