aerodynamic heating

基本解释

In this thesis, the aerodynamic heating methods of hypersonic aircrafts are presented.
本论文进行了高超声速飞行器气动热工程算法的研究。
The hypervelocity projectiles are easy to come forth aerodynamic heating and ablation phenomena, when they flight.
超高速弹箭存在的气动加热烧蚀现象会严重影响其外弹道特性。
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The phenomenon of aerodynamic heating and ablation for hypervelocity projectues seriously affects the characteristics of the exterior ballistics.
超高速弹箭存在的气动加热烧蚀现象会严重影响其外弹道特性。
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气动加热
With the rapid development of transonic and hypersonic technology, the space vehicle was forced to face severe aerodynamic heating.
随着超音速和高超音速技术的发展，严重的气动加热使空天飞行器不可避免地遭遇“热障”问题。
气动热
气动力加热

气动热
The analyses indicate that Mach number and leading edge sweep angle are important factors for aerodynamic heating.
计算结果表明,来流马赫数、前缘后掠角是影响气动热的重要因素。
空中增势