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1. 中国科学院, 长春光学精密机械与物理研究所, 应用光学国家重点实验室,吉林 长春,130033
2. 哈尔滨工业大学, 光电子技术研究所,黑龙江 哈尔滨,150001
3. 吉林大学, 物理学院,吉林 长春,130023
收稿日期:2004-06-18,
修回日期:2004-08-26,
网络出版日期:2004-10-15,
纸质出版日期:2004-10-15
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鲁建业, 王军, 马玉刚, 陈波. 纯净靶激光等离子体力学特性的理论模拟[J]. 光学精密工程, 2004,(5): 550-554
LU Jian-ye, WANG Jun, MA Yu-gang, CHEN Bo. Theoretical simulations of the mechanical characteristics of laser induced plasma for monatomic target[J]. Editorial Office of Optics and Precision Engineering, 2004,(5): 550-554
基于磁流体力学模型
对Xe、He、C、N、O、Ne、Al、Ar等元素在激光辐照下的等离子体力学特性进行了研究
并且以Al元素为例
研究了不同波长情况下的靶材烧蚀速度以及烧蚀压力的变化趋势.结果表明:在相同入射条件下
除Xe外
He、C、N、O、Ne、Al、Ar这几种元素的烧蚀压力比较接近
并且各元素的烧蚀速度的情况也大体相同
这样从增加火箭的有效载荷的角度考虑
采用大气驱动模式将是非常有利的.另外数值模拟结果还表明
随着入射光波长的增加
靶材的烧蚀速度、烧蚀压力单调下降并逐渐趋于平缓
尤其是当入射光波长小于某一个值时
这个变化非常迅速.因此
如果单纯从入射光波长角度考虑
波长越短将越有利于产生更大的推力.但短波长激光被大气散射严重
造成极大的能量损耗.因而在实际应用时
应该根据飞行器所处的不同飞行位置合理选择驱动光波长.
Based on a magneto-hydrodynamics model
the plasma characteristics for the elements Xe
He
C
N
O
Ne
Al and Ar are studied. And
numerical simulations were introduced to the relationship between the ablation-velocity and -pressure with the wavelength of the imported laser beam by using element Al as an example. These analyses show that under the same condition of the imported laser beam
the ablation-pressures and -velocities of He
C
N
O
Ne
Al and Ar are roughly equal
which means that the Air-breathing-Mode will be the profitable one to improve the effective load of the rocket. These simulations reveal that the ablation-velocity and -pressure of the target goes down and gradually tends to flatness with the increase of the imported laser wavelength. This change goes very rapidly when the wavelength is less than a certain value. If only considering the wavelengths of the induced laser beams
the shorter ones will be better to increase the thrust-force. But a laser beam with a shorter wavelength will be heavily scattered by atmosphere
leading to great energy loss. So in the practical application
the laser beam's wavelength should be chosen according to the different flying height of the aircraft.
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江少恩,刘忠礼,李楠. 激光等离子体三维重建迭代方法研究[J] . 光学精密工程,1997,5(5):36-43.JIANG S E,LIU ZH L,LI N. Numerical simulation and analysis on three-dimensional reconstruction of laser plasma[J] . Optics and Precision Engineering, 1997,5(5):36-43.(in Chinese)
KANTROWITZ, A. Propulsion to orbit by ground-based lasers[J] . Aeronautics and Astronautics, 1972, 10:74-76.
YABE T, PHIPPS C, AOKI K, et al. Laser driven vehicle[J] .SPIE, 2002, 4760:867-878.
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MASNAVI M, KIKUCHI T, NAKAJIMA M, et al. Influence of opacity on gain coefficients in static and fast moving neon-like krypton plasma[J] .J. Appl. Phys.,2002, 92(7):3480-3486.
郑力铭,朱定强,徐旭,等. 激光推进火箭发动机吸收室的数值模拟[J] . 推进技术,2002,23(5):387-390.ZHENG L M,ZHU D Q,XU X, et al. Numerical simulation of flow in the absorption chamber of laser propulsion rocket engine[J] .Journal of Propulsion Technology, 2002,23(5):387-390.(in Chinese)
李俊美,洪延姬,文明,等. 激光推进中一种光船结构的设计[J] . 装备指挥技术学院学报,2002,13(6):97-100.LI J M,HONG Y J,WEN M, et al. Structural De sign of a lightcraft for la ser propulsion[J] .Journal of the Academy of Equipment Command and Technology, 2002,13(6):97-100.(in Chinese)
张均,陈光南,常铁强. 激光产生X光的数值模拟研究[J] . 计算物理.1994,11(1):1-8.ZHANG J,CHEN G N,CHANG T Q. Investigation of numerical simulations for laser-produced X-ray[J] .Chinese Journal of Computational Physics. 1994,11(1):1-8.(in Chinese)
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