期刊文献+

吸气式激光推进中空气对CO2激光的吸收系数计算

Calculation of Absorption Coefficient of CO2 Laser by Air in Air-breathing Laser Propulsion
下载PDF
导出
摘要 比较分析了吸气式激光推进中空气对CO2激光的3种吸收机制,列出了相应的吸收系数计算公式。通过计算发现,自由-自由吸收对应的逆韧致吸收系数占总吸收系数的比例几乎达到80%,即在较强的激光辐照作用下,由于电子温度很高,高温空气主要通过逆韧致方式吸收入射激光能量。计算结果可以用于吸气式激光推进的能量沉积过程研究。 Three absorption mechanisms of CO2 laser by air in air-breathing laser propulsion are analyzed and compared,and corresponding absorption coefficient expressions are listed separately.Through calculation it is found that the proportion of inverse bremsstrahlung absorption coefficient to total absorption coefficient is almost up to 80%.That is,under stronger laser irradiation,for the electronic temperature is very high,and the incident laser energy is mainly absorbed by high-temperature air through inverse bremsstrahlung.Results of calculation can be applied in deposit process of air-breathing laser propulsion.
出处 《装备指挥技术学院学报》 2010年第3期117-119,共3页 Journal of the Academy of Equipment Command & Technology
基金 国家自然科学基金资助项目(90916015)
关键词 吸气式激光推进 CO2激光 逆韧致吸收 吸收系数 air-breathing laser propulsion CO2 laser inverse bremsstrahlung absorption absorption coefficient
  • 相关文献

参考文献10

  • 1强希文,朱润合.激光等离子体的非线性逆轫致吸收[J].激光杂志,2000,21(2):28-29. 被引量:2
  • 2强希文,张建泉,刘峰.激光等离子体的辐射与自吸收现象研究[J].激光杂志,1999,20(6):20-23. 被引量:2
  • 3WANG T S,CHEN Y S.Advanced performance modeling of experimental laser lightcrafts[C] //American Institute of Aeronautics and Astronautics.39th AIAA Aerospace Sciences Meeting & Exhibit.Reno,USA:AIAA,2001:1-11.
  • 4郑力铭,朱定强,徐旭,蔡国飙.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. 被引量:4
  • 5KATSURAYAMA H,KOMURASAKI K,ARAKAWA Y.Numerical analyses on pressure wave propagation in repetitive pulse laser propulsion[C] //American Institute of Aeronautics and Astronautics.37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.Utah,USA:AIAA,2001:1-9.
  • 6HIROOKA Y,KATSURAYAMA H,MORI K,et al.Nozzle performance of a RP laser thruster[C] //American Institute of Aeronautics and Astronautics.39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.Alabama,USA:AIAA,2003:1-7,.
  • 7HIROOKA Y,KATSURAYAMA H,MORI K,et al.Computational analysis on nozzle performance of a RP laser thruster[C] //American Institute of Aeronautics and Astronautics.42nd Aerospace Sciences Meeting & Exhibit.Reno,USA:AIAA,2004:1-6.
  • 8泽尔道维奇 Я Ъ,莱依捷尔 Ю П.激波和高温流体动力学现象物理学:上册[M].张树材,译.北京:科学出版社,1985.
  • 9MYRABO L N,RAIZER Y P.Laser-induced air spike for advanced transatmospheric vehicle[C] //American Institute of Aeronautics and Astronautics.25th AIAA Plasmadynamics and Lasers Conference.Colorado,USA,AIAA,1994:1-13.
  • 10CHUCHILL D R.Thermal radiation of phenomena[R].USA:DASA,1967:618-619.

二级参考文献6

  • 1辜建辉,徐启阳,李再光,陈殊殊.激光推进原理与技术[J].推进技术,1995,16(2):80-84. 被引量:10
  • 21,Rand S.,Phys.Rev.,1964,136:231
  • 32,Nicholson-Flourence M B.J.Phys.,1971,4:574
  • 43,Osborn R K.Phys.Rev.,1972,5:1660
  • 54,Pert G J.J.Phys.,1972,A5:1221
  • 65,Brysk H.J.Phys.,1975,A8:1260

共引文献5

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部