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激光参数对光船性能影响分析
引用本文:鄢昌渝,吴建军,刘洪刚,何振.激光参数对光船性能影响分析[J].航空学报,2009,30(2):193-199.
作者姓名:鄢昌渝  吴建军  刘洪刚  何振
作者单位:国防科学技术大学,航天与材料工程学院,湖南,长沙,410073
基金项目:国家“973”基础研究(61328);;教育部“新世纪优秀人才支持计划”(NCET-06-0927);;国防基础预研项目
摘    要: 采用三温度11组元热化学非平衡空气模型计算了激光能量在等离子体中的沉积过程,并在激光脉冲作用结束8 μs后采用平衡空气模型,完成激光推进光船工作过程的数值模拟,研究了不同入射激光能量和脉冲宽度对光船推进性能的影响。结果表明:当脉冲宽度相同时,入射激光能量越大,所得冲量耦合系数越大;当入射激光脉冲能量相同时,脉冲宽度越小,所得冲量耦合系数越大。将计算所得冲量耦合系数与Schall实验所得结果进行比较,结果非常吻合。

关 键 词:航空航天推进系统  激光推进  吸气模式  冲量耦合系数  数值模拟  

Analysis of Impact of Laser Parameters on Performance of Lightcraft
Yan Changyu,Wu Jianjun,Liu Honggang,He Zhen.Analysis of Impact of Laser Parameters on Performance of Lightcraft[J].Acta Aeronautica et Astronautica Sinica,2009,30(2):193-199.
Authors:Yan Changyu  Wu Jianjun  Liu Honggang  He Zhen
Institution:College of Aerospace and Material Engineering;National University of Defense Technology;Changsha 410073;China
Abstract:The absorptive process of laser energy in plasma is simulated by a thermo-chemical non-equilibrium air model which contained 3 temperatures and 11 species. 8 μs after the laser is terminated, the simulation is switched to an equilibrium air model to compute the operating process of a laser propulsion lightcraft. Then influences as laser energy and pulse length on the propulsive performance of the lightcraft are investigated. The results show that when the pulse length is kept equal, impulse coupling coefficient increases along with laser energy increase, while the impulse coupling coefficient increases along with the decrease of pulse length when laser energy is equal. The coupling coefficients for the lightcraft predicted by simulation agree well with those of tests done by Schall.
Keywords:aerospace propulsion system  laser propulsion  air-breathing mode  impulse coupling coefficient  numerical simulation  
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