aerodynamic heating

基本解釋

In this thesis, the aerodynamic heating methods of hypersonic aircrafts are presented.
本論文進(jìn)行了高超聲速飛行器氣動(dòng)熱工程算法的研究。
The hypervelocity projectiles are easy to come forth aerodynamic heating and ablation phenomena, when they flight.
超高速彈箭存在的氣動(dòng)加熱燒蝕現(xiàn)象會(huì)嚴(yán)重影響其外彈道特性。
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The phenomenon of aerodynamic heating and ablation for hypervelocity projectues seriously affects the characteristics of the exterior ballistics.
超高速彈箭存在的氣動(dòng)加熱燒蝕現(xiàn)象會(huì)嚴(yán)重影響其外彈道特性。
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氣動(dòng)加熱
With the rapid development of transonic and hypersonic technology, the space vehicle was forced to face severe aerodynamic heating.
隨著超音速和高超音速技術(shù)的發(fā)展，嚴(yán)重的氣動(dòng)加熱使空天飛行器不可避免地遭遇“熱障”問題。
氣動(dòng)熱
氣動(dòng)力加熱

氣動(dòng)熱
The analyses indicate that Mach number and leading edge sweep angle are important factors for aerodynamic heating.
計(jì)算結(jié)果表明,來流馬赫數(shù)、前緣後掠角是影響氣動(dòng)熱的重要因素。
空中增勢(shì)