三维尺寸对悬臂斜坡喷注器混合效率影响数值研究

  • 高峰 ,
  • 夏雪峰 ,
  • 张涵
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  • 空军工程大学防空反导学院,西安 710051

高峰(1965-),男,安徽凤阳人,教授,博士,研究方向:航空宇航推进理论与工程。

收稿日期: 2017-04-27

  网络出版日期: 2025-05-28

Numerical Study on the Effects of Three-dimensional Parameters on the Mixing Efficiency of Cantilevered Ramp Injector

  • GAO Feng ,
  • XIA Xuefeng ,
  • ZHANG Han
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  • Air and Missile Defense College, Air Force Engineering University, Xi'an 710051, China

Received date: 2017-04-27

  Online published: 2025-05-28

摘要

为分析悬臂斜坡构型对超燃燃烧室內燃料的掺混效果以及射流的穿透深度改进效果的影响,采用数值方法对不同三维尺寸的悬臂斜坡喷注器的流场情况进行模拟研究。结果表明:斜坡压缩角增大对流场的掺混效果影响不大但可以增加射流穿透深度,同时也带来更大的总压损失;后掠角度的增加可增强掺混,但也造成总压损失的增加和穿透深度的减小;悬臂宽度在一定范围内适当减小可有效增加近场的穿透深度以及远场的掺混效率,减小总压损失。

本文引用格式

高峰 , 夏雪峰 , 张涵 . 三维尺寸对悬臂斜坡喷注器混合效率影响数值研究[J]. 弹箭与制导学报, 2018 , 38(1) : 83 -88 . DOI: 10.15892/j.cnki.djzdxb.2018.01.020

Abstract

In order to analyze the impact of cantilevered ramp configuration on the mixing effect of the fuel in scramjet combustor and the improvement effect of penetration depth of jet, the numerical method was used to simulate the flow field of a cantilever ramp injector with different dimensions. The results show that the increase of the ramp compression angle has little impact on mixing effect, but it can increase the jet penetration depth and bring about a greater total pressure loss; The increase of the angle of sweepback can enhance the blending, but also increases the total pressure loss and decreases the penetration depth; The appropriate reduction of cantilever width within a certain range can effectively increase the penetration depth of near field and the mixing efficiency of far field, and reduce the total pressure loss.

参考文献

[1]
SISLIAN J P PARENT B Numerical investigation of fuel-air mixing and combustion in shcramjet inlets[J]. AIAA Journal, 2001. 399: 1698-1709.
[2]
SISLIAN J P PARENT B Numerical simulation of hypervelocity mixing and combustion in shcramjet inlets with canti-levered ramp injectors[R]. AIAA-99-4873. Reston: AIAA, 1999.
[3]
WANG Y W SISLIAN J P Numerical investigation of methane and air mixing in a scramjet inlet[R]. AIAA-2008-2533. Reston: AIAA, 2008.
[4]
SISLIAN J P PARENT B Hypervelocity fule/air mixing in a shcramjet inlet[J]. Journal of Propulsion and Power, 2004, 202: 263-272.
[5]
PARENT B SISLIAN J P Effect of geometrical paremeters on the mixing performance of cantilevered ramp injectors[J]. AIAA Journal, 2003, 413: 448-456.
[6]
PARENT B SISLIAN J P Turbulent hypervelocity fuel/air mixing by cantilevered ramp injectors[R]. AIAA-2001-4888. Reston: AIAA, 2001.
[7]
ALEXANDER D C SISLIAN J P Parent B Hypervelocity fuel/air mixing in mixed-compression inlets of shcramjets[J]. AIAA Journal, 2006, 4410: 2145-2155.
[8]
ALEXANDER D C SISLIAN J P Computational study of the propulsive characteristics of a shcramjet engine[J]. Journal of Propul and Power, 2008, 241: 34-44.
[9]
Huang Wei LI Shi-bin YAN Li Performance e-valuation and parametric analysis on cantilevered ramp in-jector in supersonic flows[J]. Acta Astronautica, 2013, 843/4: 141– 152.
[10]
毕东恒 罗世彬 林志勇 悬臂斜坡喷注器流场结构与混合特性[J]. 固体火箭技术, 2015, 381: 61-66.
[11]
毕东恒 罗世彬 林志勇 后掠结构对悬臂斜坡喷注器性能的影响[C]// 中国力学学会激波与激波管专业委员,第十六届全国激波与激波管学术会议论文集. [出版地不详]: 中国力学学会激波与激波管专业委员, 2014: 205-211.
[12]
毕东恒 罗世彬 林志勇 构型参数对悬臂斜坡喷注器混合性能的影响[J]. 推进技术, 2016, 371: 112-118.
[13]
DONOHUE J M MCDANIEL J C HAJ HARIRI H Experimental and numerical study of swept ramp injection in-to a supersonic flowfield[J]. AIAA Journal, 1994, 329: 1860-1866.
[14]
徐旭 陈兵 徐大军 冲压发动机原理及技术[M]. 北京: 北京航空航天大学出版社, 2014: 175-200.
[15]
SEGAL C MICHAEL J R The scramjet engine: proces-ses and characteristics[M]. England: Cambridge University Press, 2009: 56-73.
[16]
WEI Baoxi ZHANG Yan TIAN Liang Experimental study on combustion mode transition in an aero-ramp based scramjet[R]. AIAA-2012-3923. Reston: AIAA, 2012.
[17]
POHLMAN M R GREENDYKE R B Critical design pa-rameters for pylon-aided gaseous fuel injection[R]. AIAA-2009-4422. Reston: AIAA, 2009.
[18]
EKLUND D R GRUBER M R Study of a supersonic com-buster employing an aerodynamic ramp pilot injector[C]// AIAA. Proceedings of 35th Joint Propulsion Confer-ence and Exhibit. Reston: AIAA, 1999: 1-9.
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