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- waverider eonfiguration 乘波构型
- 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。
- Results show that: the inverse-design method for the waverider configuration is successful based on inviscid conical shock wave. 研究表明：基于无粘锥形流的乘波体气动外形的反设计方法是成功的；
- The unsteady aerodynamic characteristics of waverider 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。
- In this paper we develop a wedge-elliptical cone waverider configuration method, study on front body-scramjet engine integration design, and create a hypersonic waverider. 本文提出了一种变楔角楔/椭圆锥乘波体构型方法,并基于前体/进气道一体化设计思想,生成了高超声速乘波飞行器构型。
- As a kind of new configuration waveriders have high lift to drag ratio (L/D) in hypersonic flight, which makes the study of waverider shapes an important trend of hypersonic air vehicles development. 乘波构形在高超声速条件下的高升阻比优势备受关注，使得对于它的设计研究成为高超声速飞行器外形设计的一个重要方向。
- OPTIMIZED DESIGN OF WAVERIDER WITH HIGH LIFT OVER DRAG RATIO 高升阻比乘波构型优化设计
- Investigation of waverider configuration in hypersonic wind tunnel 乘波外形高超声速风洞测力试验研究
- 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
- 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
- Parellel Numerical Simulation of the Three-dimensional Flow Field around the Hypersonic Waverider Shape Vehicle 高超声速乘波飞行器三维流场的并行数值模拟
- Altitude and Design Length Effects of Optimized Waverider Derived from Cone Flow 飞行高度及设计长度对锥形流乘波体优化的影响
- finaneial - right eonfiguration 财权配置
- wave-rider eonfiguration 乘波构型
- eonfiguration 组态
- eonfiguration management 配置管理
- osculating cone waverider 吻切锥乘波构型
- waverider 乘波体
- waverider configuration vehicle 乘波构型飞行器
- waverider missile 乘波外形导弹
