waverider

基本解釋

A new method of quickly generating hypersonic waverider forebody configurations was developed.
發(fā)展了一種基于分析法的高超聲速乘波構(gòu)型飛行器前體設(shè)計(jì)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：基于無粘錐形流的乘波體氣動(dòng)外形的反設(shè)計(jì)方法是成功的；
The unsteady aerodynamic characteristics of waverider aircraft is one of the most important physical problems in hypersonic flight.
乘波飛行器運(yùn)動(dòng)過程中的非定常氣動(dòng)特性是高超聲速飛行中的重要物理問題之一。
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.
本文提出了一種變楔角楔/橢圓錐乘波體構(gòu)型方法,并基于前體/進(jìn)氣道一體化設(shè)計(jì)思想,生成了高超聲速乘波飛行器構(gòu)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.
乘波構(gòu)形在高超聲速條件下的高升阻比優(yōu)勢(shì)備受關(guān)注，使得對(duì)于它的設(shè)計(jì)研究成為高超聲速飛行器外形設(shè)計(jì)的一個(gè)重要方向。