内喷管单元间隙对塞锥换热的影响

韩非; 刘宇

内喷管单元间隙对塞锥换热的影响

韩非,
刘宇

北京航空航天大学宇航学院, 北京 100083

基金项目: 国家“863”基金资助项目(863-2-1-3-1)

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- 被引次数: 0
出版历程
- 收稿日期: 2007-04-04
- 修回日期: 2007-11-21
- 刊出日期: 2008-04-28

Effects of gap between nozzles on plug heat transfer characteristics

HAN Fei,
LIU Yu

School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

摘要

摘要: 为了解内喷管单元间隙对塞锥换热的影响,建立塞式喷管发动机的三维计算模型,采用数值模拟的方法对不同背压不同冷却剂流量下的塞锥进行换热研究,得出不同工况下的冷却剂温升、压降以及壁面温度、压强和热流密度的分布情况,其中着重研究了内喷管单元间隙对塞锥换热的影响.计算结果表明:由于受单元间隙的影响,造成沿宽度方向上塞锥壁面的压强、热流密度和温度的大小分布不均,并且随着环境压强的降低,单元间隙的影响有减弱趋势.
- 航空、航天推进系统 /
- 液体推进剂火箭发动机 /
- 塞式喷管 /
- 再生冷却 /
- 数值模拟
Abstract: To understand the effects of gap between nozzles on plug heat transfer characteristics,three dimension computational models of plug nozzle were established and studied numerically.Heat transfer characteristics of plug with different ambient pressure and different coolant flow rate were investigated.The results of coolant heat pick-up and pressure loss,wall temperature,pressure and heat flux distribution were obtained,especially the effects of gap between nozzles on plug heat transfer characteristics.The results show that: due to the effect of gap between nozzles,the distribution of pressure,heat flux and temperature along the width of plug is different.With decrease of ambient pressure,this effect becomes weaker.
- aerospace propulsion system /
- liquid propellant rocket engines /
- plug nozzle /
- regenerative cooling /
- numerical simulation

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参考文献(4)

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[2]	Wang T S.Analysis of linear aerospike plume-induced X-33 base-heating environment[J].Journal of Spacecraft and Rockets,1999,36(6):777-783.
[3]	Kumakawa A,Tomita T.A study of plug-nozzle rocket calorimeters[R].AIAA 96-2583,1996.
[4]	李军伟,刘宇,覃粒子.二维塞式喷管再生冷却换热的数值模拟[J].航空动力学报,2005,20(1):147-153.LI Junwei,LIU Yu,QIN Lizi.Numerical simulation of regenerative cooling in two dimensional plug nozzles[J].Journal of Aerospace Power,2005,20(1):147-153.