transient aerodynamic heating

基本解釋

A high speed and accurate E T translation method of sensor for transient aerodynamic heating control system of high speed flight vehicle is proposed.
提出一種高速飛行器瞬態(tài)氣動加熱控制系統(tǒng)中傳感器的快速、高精度“E T”轉(zhuǎn)換方法。
A numerical method was presented for transient heat transfer processes in honeycomb sandwich panels used in metallic thermal protection systems (TPS) under aerodynamic heating.
提出一種計算非穩(wěn)態(tài)氣動加熱下金屬蜂窩板內(nèi)輻射導熱耦合換熱數(shù)值計算方法。
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.
對某種金屬蜂窩平板進行了模擬氣動加熱試驗，測定了加熱表面和非加熱表面的瞬態(tài)溫度。