首页 | 本学科首页   官方微博 | 高级检索  
     检索      

塞锥截短对塞式喷管性能影响的实验
引用本文:王一白,覃粒子,刘宇,王长辉.塞锥截短对塞式喷管性能影响的实验[J].北京航空航天大学学报,2008,34(1):13-16.
作者姓名:王一白  覃粒子  刘宇  王长辉
作者单位:北京航空航天大学 宇航学院, 北京 100083
基金项目:国家高技术研究发展计划(863计划)
摘    要:为了研究塞锥截短对塞式喷管性能的影响,对截短率为80%、40%、30%和20%的塞式喷管进行了冷流实验.介绍了实验系统的组成和推力测量方式,得到了不同塞锥截短率的推力系数效率的高度特性曲线.实验结果表明:截短率越小,效率越低,不同截短率的效率差别随着压强比的增加而减小;随着截短率增大,截短率对效率的影响程度逐渐降低.截短率太小,性能损失较大;截短率太大,塞锥的尺寸增大,而性能提高却不明显.通常的取值范围是30%~40%.

关 键 词:塞式喷管  推力系数效率  截短率
文章编号:1001-5965(2008)01-0013-04
收稿时间:2007-01-15
修稿时间:2007年1月15日

Effects of truncation on thrust performance of aerospike nozzles
Wang Yibai,Qin Lizi,Liu Yu,Wang Changhui.Effects of truncation on thrust performance of aerospike nozzles[J].Journal of Beijing University of Aeronautics and Astronautics,2008,34(1):13-16.
Authors:Wang Yibai  Qin Lizi  Liu Yu  Wang Changhui
Institution:School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
Abstract:To discuss the performance effects of plug truncation ratios,cold-flow tests were performed for 80%,40%,30% and 20% truncated aerospike nozzles by employing cold air as propellant.The test system apparatus and thrust measurement were introduced.The experimental altitude characteristics curves of the thrust coefficient efficiency were obtained.The results show that the efficiency of aerospike nozzles with bigger truncation ratios is higher than with smaller ratios,and the distinction of different truncations was minished with the pressure ratio increasing.The influence degree of the truncation on the thrust coefficient efficiency falls down by increasing the ratio.The performance loss is more due to selecting too small value of the truncation ratio.With too big ratio value the length of plug is much long,and the weight of plug increases much,but the nozzle performance elevates a little.Generally the truncation ratios can be chosen from 30% to 40%.
Keywords:aerospike nozzle  thrust coefficient efficiency  truncation ratio
本文献已被 CNKI 维普 万方数据 等数据库收录!
点击此处可从《北京航空航天大学学报》浏览原始摘要信息
点击此处可从《北京航空航天大学学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号