乘波

网络释义

1.
waverider
X-30的气动外形采用了“乘波”(waverider)设计，升力多来自机身的压缩冲程，“机翼”面积很小仅提供姿态控制。这种外形比较利 …
article.yeeyan.org|基于5个网页
2.
Ride Wave
该计划研究的核心部分是一种呈后掠的“乘波”(Ride Wave) 构型的实验飞行器，它能以M≥5的速度飞行，装有GPS定位系统、收 …
iask.sina.com.cn|基于 1 个网页

例句

释义:
全部全部,waveriderwaverider,Ride WaveRide Wave
类别:全部全部,口语口语,书面语书面语,标题标题,技术技术
来源:全部全部,字典字典,网络网络
难度:全部全部,简单简单,中等中等,难难
1.
This method can be applied to pre-research and multi-objective optimization design of hypersonic QWV.
该方法可应用于高超声速类乘波体飞行器的概念研究和多目标优化设计。
www.ceps.com.tw
2.
The unsteady aerodynamic characteristics of wave rider aircraft is one of the most important physical problems in hypersonic flight.
乘波飞行器运动过程中的非定常气动特性是高超声速飞行中的重要物理问题之一。
www.dictall.com
3.
In this paper, the forced rolling movement about the symmetry axis at a fixed angle of attack is numerically simulated.
采用数值模拟方法模拟了乘波飞行器在固定迎角下绕其对称轴强迫滚转运动这一过程。
hkxb.buaa.edu.cn
4.
A new method of quickly generating hypersonic waverider forebody configurations was developed.
发展了一种基于分析法的高超声速乘波构型飞行器前体设计方法。
www.dictall.com
5.
The favorable method of improving the lift-drag ratio of the figuration is brought forward.
分析提出了进一步提高该乘波体气动布局升阻比的有效途径。
bhxb.buaa.edu.cn
6.
Design and computational study of waverider configuration with high performance
高升阻比乘波体外形设计及气动特性计算研究
www.ilib.cn
7.
Trajectory Characteristics of Hypersonic Waverider Missile with Rocket Extended Range
火箭增程乘波外形导弹弹道特性研究
www.ilib.cn
8.
Optimized design of waverider forebody derived from asymmetric near-isentropic compression flow fields
轴对称近似等熵压缩流场的乘波前体优化设计
www.ilib.cn
9.
An aerodynamic experiment research of the hypersonic waverider vehicle
高超声速乘波飞行器气动实验研究
www.ilib.cn
10.
Cone-derived Waverider Configuration Design and Performance Research
锥导乘波机的构型设计与性能研究
www.ilib.cn