You want to give him a teddy bear?

1、

Definitely one teddy bear that every little girl wishes for.

毫无疑问这是每个小女孩都想要的泰迪熊。

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2、

Who wants the teddy bear with one leg?

谁要一只脚的泰迪熊？

provided by jukuu

3、

A robot's appearance affects its ability to successfully interact with humans, which is why the RIKEN-TRI Collaboration Center for Human-Interactive Robot Research decided to develop a robotic nurse that looks like a huge teddy bear.

机器人的外观影响其与人类成功交互的能力，这就是为什么RIKEN-TRI人机交互研究合作中心决定开发一个外表像大泰迪熊的机器人护士的原因。

六级真题- 2018年 12月 2卷阅读B

4、

This teddy bear is similar to that one.

这个玩具熊和那个相似。

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5、

Sure. How about this Teddy Bear wrapping paper?

当然可以。这张玩具熊包装纸怎么样？

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6、

Chaos characteristics of the aerodynamic noise are discussed and the aeroacoustic noise signals on helicopter scissors tail rotor is analyzed by the chaos theory.

直升机尾桨/尾梁耦合稳定性分析研究研究剪刀式尾桨气动噪声的混沌特性，并应用混沌理论进行了直升机尾桨气动噪声信号分析。

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7、

The range of yawing rate when turning left in hover is calculated, where the tail rotor might get into vortex ring.

根据右侧飞试验结果，估算出样机悬停回转时尾桨处于涡环状态的偏航角速度范围；

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8、

A free wake analytical model is then developed for predicting the aerodynamic characteristics of a scissors tail rotor and validated by numerical examples.

然后，建立了一个剪刀式尾桨气动特性计算的分析模型，并进行了验证。

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9、

CFD Simulation and Validation of Ducted Tail Rotor Numerical Simulation and Validation of Wake Field of Submarine with Stern Appendage

涵道尾桨的CFD模拟与验证带附体潜艇尾流场的数值模拟与验证

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10、

Last, by contrastive analysis between the results of the isolated tail rotor noise and the experiment, the computation model is being proven.

最后将孤立尾桨噪声的计算结果和试验结果进行了对比分析，验证了计算模型。

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11、

The machined self lubricating composite tail rotor gears will stand up to the most aggressive 3D flying.

悬停状态下直升机尾桨/尾梁耦合动力稳定性分析加工自润滑复合材料尾桨齿轮都会挺身而出最具侵略性3D飞行。

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12、

We have a tail rotor de-ice caution light.

我们的机尾结冰警示灯报警。

provided by jukuu

13、

These conclusions can be used to estimate the helicopter tail rotor noise and help to guide tail rotor noise reduction design.

这些结论为预估直升机的尾桨噪声和指导降低噪声尾桨设计提供了依据。

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14、

The flow field characteristic of a helicopter ducted tail rotor in hovering were analyzed using CFD method in this paper.

本文采用CFD方法分析了悬停状态下涵道尾桨的流场特性。

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15、

An experimental and analytical investigation on the aerodynamic characteristics of a helicopter scissors tail rotor has been made.

对剪刀式尾桨的气动特性进行了实验和分析研究。

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16、

This article describes dynamic stress measurement of x-type of helicopter tail rotor tunnel test in several principal aspects.

本文介绍x型直升飞机尾桨吹风试验动应力测量工作的几个主要方面。

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17、

Difference of prepreg technique and the tail rotor rigidity were the key resulting in product life decline.

预浸料工艺性能的差异及桨叶刚度不足是造成产品寿命下降的主要原因。

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18、

In the transmission system of the helicopter, it is very important to transmit power to the tail rotor.

直升机动力传动系统中，尾传动系统是其重要的组成部分。

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19、

This paper introduces a method of making selection of helicopter tail rotor parameter optimization using computer optimum techniques.

本文介绍采用计算机优化技术进行直升机尾桨参数优化选择的方法。

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20、

CFD Analysis for the Ducted Tail Rotor Based on Momentum-Source Method

基于动量源方法的涵道尾桨CFD分析

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