Temporal response in the emission spectrum of detonation processes and the measurement of detonation temperature is studied.
研究爆轰反应过程的光谱时间响应特性并测量爆温。
The main works of this paper are about the measurement of the detonation temperature and the internal structure of reaction zone of explosives, which are summarized as follows: 1.
本文主要从以下几个方面对高能炸药爆温及反应区结构进行了研究：1。
According to the principle of optical temperature measurement, how to use a pyrometer to measure the temperature of detonation products in experiment is described.
根据光学测温原理，介绍了如何在实验中用高温计实现爆轰产物温度的测量。
The thermal equilibrium time of wall temperature decreases linearly with the detonation frequency increasing.
壁温分布热平衡时间随爆震频率的升高而减小，且基本上呈线性关系。
A pulse detonation rocket engine (PDRE) is a new propulsion system that generates thrust by using high-temperature and high-pressure air produced by pulse detonation waves.
脉冲爆震火箭发动机是一种利用脉冲式爆震波产生高温、高压燃气发出的冲量来产生推力的新型推进系统。
A method of simultaneously measuring detonation velocity and temperature, or detonation pressure and temperature by optical technique is presented in this paper.
本文介绍了一种用光电技术同时测定爆速和爆温、爆压和爆温的方法。
This paper is mainly concerned with the oxygen hydrogen detonation driving technique, which is used in JF-10 shock tunnel to explore the high temperature real gas effects on heat transfer.
本文主要介绍了爆轰波驱动技术在激波风洞实验方面的应用。首先，JF-10高焓激波风洞，经过努力成功地实现带扩容腔的变截面氢氧爆轰方式运行。
This paper is mainly concerned with the oxygen hydrogen detonation driving technique, which is used in JF-10 shock tunnel to explore the high temperature real gas effects on heat transfer.
本文主要介绍了爆轰波驱动技术在激波风洞实验方面的应用。首先，JF-10高焓激波风洞，经过努力成功地实现带扩容腔的变截面氢氧爆轰方式运行。
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