waverider

常見(jiàn)例句

• 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(wú)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(guò)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(wèn)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。
• OPTIMIZED DESIGN OF WAVERIDER WITH HIGH LIFT OVER DRAG RATIO
  高升阻比乘波構(gòu)型優(yōu)化設(shè)計(jì)
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