transient aerodynamic heating

基本解释

A high speed and accurate E T translation method of sensor for transient aerodynamic heating control system of high speed flight vehicle is proposed.
提出一种高速飞行器瞬态气动加热控制系统中传感器的快速、高精度“E T”转换方法。
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。