超级军网鸡光还能有这种搞法，磨想到
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涡轮喷气CO2气动激光器概念研究
王建，陈建平，刘小军，顾婷婷
（北京航空工程技术研究中心 第3研究室，北京 100076）
摘要：通过分析航空发动机和燃烧驱动CO2气动激光器的相似性，探讨了将航空发动机改装成CO2气动激光器的可行性.提出了涡轮喷气CO2气动激光器的概念和基本框架，分析了其中涉及的各项关键技术和初步解决方案.针对典型航空发动机的工作状态，设计了阵列喷管型面，并对小信号增益和喷管内流场分布进行了数值计算.结果表明，利用航空发动机燃气可以获得较高的小信号增益，涡轮喷气CO2气动激光器存在其合理性和可行性.
关键词：航空发动机；气动激光器；小信号增益；流场分布；数值计算
中图分类号：V239文献标识码：A
Conception research of CO2 gasdynamic laser based on turbojet
WANG Jian，CHEN Jianping，LIU Xiaojun，GU Tingting
（The 3rd Research Office,
Beijing Aeronautical Technology Research Center，Beijing 100076，China）
Abstract：The combustion driven CO2 gasdynamic laser （GDL） is similar with advanced aeroengine. The possibility of refitting a CO2 GDL from an aeroengine was discussed here,then the conception, basic frame and key techniques were analyzed. A nozzle figure was designed in allusion to the typical working condition of aeroengine, small signal gain and flow field distribution were calculated primarily. The result that high small signal gain is achieved shows that CO2 GDL based on the turbojet is possible.
Key words: aeroengine;gasdynamic laser;small signal gain;flow field distribution;numerical calculation涡轮喷气CO2气动激光器概念研究
王建，陈建平，刘小军，顾婷婷
（北京航空工程技术研究中心 第3研究室，北京 100076）
摘要：通过分析航空发动机和燃烧驱动CO2气动激光器的相似性，探讨了将航空发动机改装成CO2气动激光器的可行性.提出了涡轮喷气CO2气动激光器的概念和基本框架，分析了其中涉及的各项关键技术和初步解决方案.针对典型航空发动机的工作状态，设计了阵列喷管型面，并对小信号增益和喷管内流场分布进行了数值计算.结果表明，利用航空发动机燃气可以获得较高的小信号增益，涡轮喷气CO2气动激光器存在其合理性和可行性.
关键词：航空发动机；气动激光器；小信号增益；流场分布；数值计算
中图分类号：V239文献标识码：A
Conception research of CO2 gasdynamic laser based on turbojet
WANG Jian，CHEN Jianping，LIU Xiaojun，GU Tingting
（The 3rd Research Office,
Beijing Aeronautical Technology Research Center，Beijing 100076，China）
Abstract：The combustion driven CO2 gasdynamic laser （GDL） is similar with advanced aeroengine. The possibility of refitting a CO2 GDL from an aeroengine was discussed here,then the conception, basic frame and key techniques were analyzed. A nozzle figure was designed in allusion to the typical working condition of aeroengine, small signal gain and flow field distribution were calculated primarily. The result that high small signal gain is achieved shows that CO2 GDL based on the turbojet is possible.
Key words: aeroengine;gasdynamic laser;small signal gain;flow field distribution;numerical calculation
王建，陈建平，刘小军，顾婷婷
（北京航空工程技术研究中心 第3研究室，北京 100076）
摘要：通过分析航空发动机和燃烧驱动CO2气动激光器的相似性，探讨了将航空发动机改装成CO2气动激光器的可行性.提出了涡轮喷气CO2气动激光器的概念和基本框架，分析了其中涉及的各项关键技术和初步解决方案.针对典型航空发动机的工作状态，设计了阵列喷管型面，并对小信号增益和喷管内流场分布进行了数值计算.结果表明，利用航空发动机燃气可以获得较高的小信号增益，涡轮喷气CO2气动激光器存在其合理性和可行性.
关键词：航空发动机；气动激光器；小信号增益；流场分布；数值计算
中图分类号：V239文献标识码：A
Conception research of CO2 gasdynamic laser based on turbojet
WANG Jian，CHEN Jianping，LIU Xiaojun，GU Tingting
（The 3rd Research Office,
Beijing Aeronautical Technology Research Center，Beijing 100076，China）
Abstract：The combustion driven CO2 gasdynamic laser （GDL） is similar with advanced aeroengine. The possibility of refitting a CO2 GDL from an aeroengine was discussed here,then the conception, basic frame and key techniques were analyzed. A nozzle figure was designed in allusion to the typical working condition of aeroengine, small signal gain and flow field distribution were calculated primarily. The result that high small signal gain is achieved shows that CO2 GDL based on the turbojet is possible.
Key words: aeroengine;gasdynamic laser;small signal gain;flow field distribution;numerical calculation涡轮喷气CO2气动激光器概念研究
王建，陈建平，刘小军，顾婷婷
（北京航空工程技术研究中心 第3研究室，北京 100076）
摘要：通过分析航空发动机和燃烧驱动CO2气动激光器的相似性，探讨了将航空发动机改装成CO2气动激光器的可行性.提出了涡轮喷气CO2气动激光器的概念和基本框架，分析了其中涉及的各项关键技术和初步解决方案.针对典型航空发动机的工作状态，设计了阵列喷管型面，并对小信号增益和喷管内流场分布进行了数值计算.结果表明，利用航空发动机燃气可以获得较高的小信号增益，涡轮喷气CO2气动激光器存在其合理性和可行性.
关键词：航空发动机；气动激光器；小信号增益；流场分布；数值计算
中图分类号：V239文献标识码：A
Conception research of CO2 gasdynamic laser based on turbojet
WANG Jian，CHEN Jianping，LIU Xiaojun，GU Tingting
（The 3rd Research Office,
Beijing Aeronautical Technology Research Center，Beijing 100076，China）
Abstract：The combustion driven CO2 gasdynamic laser （GDL） is similar with advanced aeroengine. The possibility of refitting a CO2 GDL from an aeroengine was discussed here,then the conception, basic frame and key techniques were analyzed. A nozzle figure was designed in allusion to the typical working condition of aeroengine, small signal gain and flow field distribution were calculated primarily. The result that high small signal gain is achieved shows that CO2 GDL based on the turbojet is possible.
Key words: aeroengine;gasdynamic laser;small signal gain;flow field distribution;numerical calculation
TG V5
论文，只是论文，一种思路
楼主论文党。。。佩服佩服
henka123 发表于 2011-3-4 22:32 
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佩服个毛啊
[/quo佩服个毛啊
只是论文
楼主有心。只是这些都是公开发表的论文吗？还是内部刊物啊？继续潜伏。。。。。。
列兵确实威武！
TG V5
思路广 欢乐多
论文是最可靠的。其一：高级别专业人士撰写，比不明身份人士所谓爆尿可靠。其二：现下的学术体制，中青年专家都得有学术成就，不管负责什么项目，有成果了甚至只是有靠得住的想法了都想形成论文，隐姓埋名的邓稼先现在找不到的，当然涉密内容要隐晦、要刊发在体制内权威刊物上。其三即便仅是设想阶段，也不是想到什么就敢瞎写的，起码实验室里要忙活一阵，这个学理科的都知道，又不是写小说。因此本座喜欢搜集筛选论文。别什么词后面都加个党字，哪个词后面加不了党字，以为加个党字就把别人鄙视到位了？
文献帝~~
梅兰竹菊 发表于 2011-3-4 22:35
看了你下面的回复，我表示没有任何恶意哈，别激动~和爬墙党，酒桌党什么的一样，都是消息来源而已
看了你下面的回复，我表示没有任何恶意哈，别激动~和爬墙党，酒桌党什么的一样，都是消息来源而已