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复合推进剂实际点火过程的实验研究 被引量:1
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作者 李逢春 张富升 雷凡培 《固体火箭技术》 EI CAS CSCD 1989年第4期39-44,共6页
固体火箭发动机的实际点火过程是极为复杂的,它不但是个瞬变过程,而且还是包括对流、导热和辐射传热过程等的复杂的物理化学过程,为了形象地揭示固体火箭发动机的实际点火过程,本文作者设计了带透明窗的小型点火试验发动机装置,采用高... 固体火箭发动机的实际点火过程是极为复杂的,它不但是个瞬变过程,而且还是包括对流、导热和辐射传热过程等的复杂的物理化学过程,为了形象地揭示固体火箭发动机的实际点火过程,本文作者设计了带透明窗的小型点火试验发动机装置,采用高频响压力传感器、光电管和高速摄影,利用同步控制装置,极为准确地记录了这一过程。 展开更多
关键词 固体推进剂点火 复合推进剂 实验设计 照相记录系统
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Ignition models and simulation of solid propellant of thermodynamic undersea vehicle 被引量:1
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作者 ZHANG Jin-jun QIAN Zhi-bo YANG Jie YAN Ping 《Journal of Marine Science and Application》 2007年第2期30-36,共7页
The starting characteristics of thermodynamic undersea vehicle systems are determined by the geometry, size and combustion area of solid propellants, which directly effect liquid propellant pipeline design. It is nece... The starting characteristics of thermodynamic undersea vehicle systems are determined by the geometry, size and combustion area of solid propellants, which directly effect liquid propellant pipeline design. It is necessary to establish accurate burning models for solid propellants. Based on combustion models using powder rings and two different solid ignition grains, namely star-shaped ignition grains and stuffed ignition grains, a mathematic model of the ignition process of the propulsion system was built. With the help of Matlab, a series of calculations were made to determine the effects of different grains on ignition characteristics. The results show that stuffed ignition grain is best suited to be the ignition grain of a thermodynamic undersea vehicle system. 展开更多
关键词 THERMOLOGY undersea vehicle solid ignition grain burning model starting process thermal power system
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Gas dynamics and heat transfer inside a solid propellant crack during ignition transient 被引量:3
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作者 LIU DongQing SUN Bing ZHANG JianWei 《Science China(Technological Sciences)》 SCIE EI CAS 2014年第11期2220-2230,共11页
To study the gas dynamic and heat transfer phenomena inside a single isolated longitudinal solid propellant surface crack,two3-D geometric models with different crack shapes were constructed.Concerning the influence o... To study the gas dynamic and heat transfer phenomena inside a single isolated longitudinal solid propellant surface crack,two3-D geometric models with different crack shapes were constructed.Concerning the influence of propagation of jet from the igniter on the flame spreading phenomena in the crack,flow region around the opening of the crack was also included in the above geometric models.A theoretical framework was then adopted to model the conjugate heat transfer in the combustion channel and the crack cavity.Numerical simulation results indicate that the ignition shock wave can spread into the crack cavity.Extremely high overpressure and pressurization rate were observed along the crack front.It is possible that the crack may propagate before the flame front reaches it.An ignited region located at the crack front near to the channel surface in downstream direction was generated long before the flame front reached the crack opening in both models. 展开更多
关键词 solid propellant CRACK shock wave conjugate heat transfer flame spreading
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