基于准静态波的吸气式高重频脉冲激光推进性能数值研究  

Numerical study on performance of air-breathing high frequency pulsed laser propulsion

作　　者：李倩 洪延姬 杨鹏涛[2] 柯发伟[3] 

机构地区：[1]装备学院,北京101416 [2]中国酒泉卫星发射中心,甘肃酒泉732750 [3]中国空气动力研究与发展中心,四川绵阳621000

出　　处：《强激光与粒子束》2011年第9期2282-2286,共5页High Power Laser and Particle Beams

基　　金：国家自然科学基金项目(90916015)

摘　　要：根据高重频脉冲激光产生光学脉冲放电形成准静态波的原理,对自编的流体力学计算程序进行了验证,结果表明该程序可用于吸气式高重频脉冲激光推进性能的数值研究。分别计算了基于移动点火点和喷射气流两种模式下准静态波流场的冲量耦合系数,均高达600N/MW,比传统的低频脉冲激光推进冲量耦合系数250N/MW高。比较了两种模式的优缺点,给出了不同模式的适用情况,结果表明,对于机理研究来说,喷气模式更易于实现。Based on the mechanism of quasi-stationary wave（QSW） formed by optical pulsed discharge（OPD）,which is generated by high frequency pulsed laser,a self-compiled computational fluid dynamics program is validated.The results indicate that this program can be used to study air-breathing high frequency pulsed laser propulsion numerically.Impulse coupling coefficients of QSW fluid field based on moving igniting point mode and jet flow mode are both up to about 600 N/MW,which are higher than that of traditional low frequency pulsed laser propulsion（250 N/MW）.Advantages and disadvantages of the two modes are compared,and their applicable situation is listed.Moreover,the jet flow mode is easier to realize for mechanism study.

关 键 词：高重频脉冲激光推进 光学脉冲放电 准静态波 数值研究 

分 类 号：TN249[电子电信—物理电子学] V439[航空宇航科学与技术—航空宇航推进理论与工程]