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乘波

网络waverider; Ride Wave

乘波

乘波

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 …

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 …

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。

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。

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。

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。

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

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

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

10

Cone-derived Waverider Configuration Design and Performance Research

锥导乘波机的构型设计与性能研究

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