In this thesis, the aerodynamic heating methods of hypersonic projectile are presented.
本论文进行了高超声速弹丸的气动热研究。
Hence, it was necessary to devise a heat shield to protect it against this intense aerodynamic heating.
因此，有必要制做一个隔热板，以防止这种强烈的气动力加热。
A set of experimental results is provided in this paper. Some problems of aerodynamic heating and flowing phenomenon are analysed.
本文提供了一组实验结果，并进行了气动加热与流动现象分析。
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。
Under the combined action of aerodynamic pressure and aerodynamic heating, the skin panels of these vehicles can undergo extremely complicated flutter motion.
在空气动力压力和空气动力加热的综合作用下，这些表面板可以承受极其复杂的震颤运动。
Because of the drastic aerodynamic heating effect, panel flutter analysis considering thermal effects becomes an emerging problem in the design process of supersonic aircraft.
在超音速飞行器的设计中，由于气动加热效应相当剧烈，考虑热效应的壁板颤振问题成为一个不可忽视的气动弹性问题。
A numerical method was presented for transient heat transfer processes in honeycomb sandwich panels used in metallic thermal protection systems (TPS) under aerodynamic heating.
提出一种计算非稳态气动加热下金属蜂窝板内辐射导热耦合换热数值计算方法。
An aerodynamic heating simulation test was carried out on a metallic honeycombed plate and the transient surface temperatures of the heating and UN heating surface were obtained.
对某种金属蜂窝平板进行了模拟气动加热试验，测定了加热表面和非加热表面的瞬态温度。
From the characteristics of aerothermoelasticity, the effects of temperature in aerodynamic heating on the mode of a delta wing and the characteristic of its flutter were researched.
根据热气动弹性特点，探讨了气动加热温度对三角机翼模态特性和颤振特性的影响。
This paper calculates the temperature distribution in plate frame of fuselage subjected to aerodynamic heating by means of the former three methods. The numerical results turn out to compare f…
本文用前三种方法计算受气功加热的机身实心框的温度分布，井与全尺寸试验结果比较，得出满意的结果。这说明文中采用的各种处理方法是可行的。
Thermal stress in meteoroids by aerodynamic heating is calculated for the ideal case of an isotropic, homogeneous, elastic sphere being heated at the surface with a constant heat transfer coefficient.
对在一个各向同性、均匀的弹性球的具有恒定的热传导系数的球面上进行加热这一理想情况下，计算了陨星由于空气动力学加热而产生的热应力。
Thermal stress in meteoroids by aerodynamic heating is calculated for the ideal case of an isotropic, homogeneous, elastic sphere being heated at the surface with a constant heat transfer coefficient.
对在一个各向同性、均匀的弹性球的具有恒定的热传导系数的球面上进行加热这一理想情况下，计算了陨星由于空气动力学加热而产生的热应力。
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