利用矩形激波管测定了几种碳氢燃料与空气混合物的爆轰极限和临界起爆能。
This paper measured the critical energy and detonation limit of hydrocarbon and air mixtures in the rectangle shock tube.
本研究是用实验观测的方法判明低密度空气中发生的强激波的构造并进而分析其特性。
The research tries to distinguish structure of strong shock-wave generated in low-density air by means of test and observation, and then analyse its characteristics.
惰性物质悬浮于空气中形成的云雾(例如水雾)能阻挡或抑制火焰和激波传播。
The cloud (such as water cloud), which is formed by the inert substance suspending in the air, can prevent or suppress flame and shock wave's propagation.
提出一种基于激波管实验和理论的空气袋织物透气率的测试方法。
A method based on the shock tube experiment is proposed for measuring the permeability of airbag fabrics.
通过采用线线合成光谱的方法得到激波后不同时刻高温空气中OH分子的转动温度。
The rotational temperatures were determined using fits to synthetic OH molecular spectra at different time behind shock waves.
采用双波长双脉冲激光全息术，对有激波存在下的空气放电现象进行了研究。
This thesis adopted two-wavelength double pulses laser holographic interferometry to study the air discharge in a shock wave field.
此外，由燃烧驱动激波管产生的高温燃气作为引导火焰点燃激波风洞产生的预混与预热的超声速碳氢燃料——空气混合物。
In addition, a hot, burned gas generated from the shock tube was used as pilot flame for igniting the premixed and preheated supersonic hydrocarbon-air mixture generated in the shock tunnel.
采用激波风洞-激波管组合设备对预混的碳氢燃料——空气混合物的点火与超声速燃烧进行了研究。
A combination facility, which consists of a shock tunnel and a shock tube, was used for studying ignition and supersonic combustion of premixed hydrocarbon fuel-air mixture.
采用激波风洞-激波管组合设备对预混的碳氢燃料——空气混合物的点火与超声速燃烧进行了研究。
A combination facility, which consists of a shock tunnel and a shock tube, was used for studying ignition and supersonic combustion of premixed hydrocarbon fuel-air mixture.
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