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不同延伸段压力分布的双钟形喷管设计
引用本文:刘亚洲,李平,陈宏玉,杨建文,陈一丹.不同延伸段压力分布的双钟形喷管设计[J].航空动力学报,2022,37(2):424-432.
作者姓名:刘亚洲  李平  陈宏玉  杨建文  陈一丹
作者单位:1.西安航天动力研究所 液体火箭发动机技术重点实验室,西安 710100
基金项目:液体火箭发动机技术重点实验室开放基金(HTKJ2020KL011005)
摘    要:针对不同延伸段压力分布的双钟形喷管,采用特征线法,分别对最大推力、等压分布及等逆压梯度分布的延伸段型面开展了设计,通过仿真手段对设计方法进行了校验,并对不同延伸段压力分布的双钟形喷管工作过程开展了研究.结果表明:最大推力及已知壁面压力的反设计方法能够实现特定压力分布的延伸段型面设计.延伸段逆压梯度分布的双钟形喷管能够在...

关 键 词:双钟形喷管  特征线法  延伸段型面设计  流动分离  模态转换
收稿时间:2021/3/6 0:00:00

Design of dual-bell nozzles with different extension pressure distributions
LIU Yazhou,LI Ping,CHEN Hongyu,YANG Jianwen,CHEN Yidan.Design of dual-bell nozzles with different extension pressure distributions[J].Journal of Aerospace Power,2022,37(2):424-432.
Authors:LIU Yazhou  LI Ping  CHEN Hongyu  YANG Jianwen  CHEN Yidan
Institution:1.Science and Technology on Liquid Rocket Engine Laboratory,Xi'an Aerospace Propulsion Institute,Xi'an 710100,China2.Academy of Aerospace Propulsion Technology,China Aerospace Science and Technology Corporation,Xi'an 710100,China
Abstract:For dual-bell nozzles with different extension pressure distribution,the method of characteristics was used to design the maximum thrust,constant pressure distribution,and positive gradient pressure distribution's extended contours.Then design methods were verified by simulation,and the operating processes of dual-bell nozzles with different extension pressure distributions were investigated.Results showed that,extended contours with specific pressure distributions could be designed by the maximum thrust and reverse design method with wall pressure known.Modes transition time of dual-bell nozzles with extensions positive gradient pressure distribution was less than engine start-up,but time of models with extensions negative gradient pressure and constant pressure distribution was longer.Compared with the maximum thrust contour,dual-bell nozzles with extension positive gradient pressure distribution had some performance loss.When extension pressure rising value was 0.001 5 time combustion chamber pressure,the average specific impulse dropped by 0.44%. 
Keywords:dual-bell nozzles  method of characteristics  extend contour design  flow separation  modes transition
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