waverider

基本解释

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。