ROCKETS TECHNOLOGY

Influence of Primary Rocket Location along the Flow-patch on the Performance of RBCC at Sea-level Static

  • WU Yake ,
  • XU Weichang ,
  • HUANG Wei ,
  • HU Zongchun ,
  • LIU Xiaowei ,
  • SHI Lei
Expand
  • 1 Sergeant College, Rocket Force Engineering University, Shandong Qingzhou 262500, China
    2 Xi'an Aerospace Propulsion Institute, CASC, Xi'an 710100, China
    3 Northwestern Polytechnical University, Xi'an 710072, China

Received date: 2016-11-17

  Online published: 2025-05-22

Abstract

Influence of primary rocket location along the flow-patch on the performance of RBCC at sea-level static was researched by CFD on an inlet-combustor combined RBCC structure. It is concluded that the influence of moving primary rocket along the flow-patch backward on intake performance is very complicated and closely bound up with the mass flow rate of primary rocket. However, moving primary rocket backward has always positive influence on the RBCC thrust and specific impulse. Moving primary rocket as backward as possible at sealevel static is recommended to maintain optimal performance of the RBCC engine.

Cite this article

WU Yake , XU Weichang , HUANG Wei , HU Zongchun , LIU Xiaowei , SHI Lei . Influence of Primary Rocket Location along the Flow-patch on the Performance of RBCC at Sea-level Static[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2017 , 37(5) : 91 -94,98 . DOI: 10.15892/j.cnki.djzdxb.2017.05.021

References

[1]
王国辉 火箭基组合循环(RBCC)引射模态工作过程研究[D]. 西安: 西北工业大学, 2001.
[2]
刘佩进 RBCC引射火箭模态性能与影响因素研究[D]. 西安: 西北工业大学, 2001.
[3]
黄生洪 火箭基组合循环(RBCC)引射模态燃烧流动研究[D]. 西安: 西北工业大学, 2002.
[4]
刘洋 RBCC引射/亚燃及其模态过渡工作过程研究[D]. 西安: 西北工业大学, 2008.
[5]
李宇飞 RBCC引射/亚燃模态热力调节机理研究[D]. 西安: 西北工业大学, 2008.
[6]
吕翔 RBCC 推进系统总体设计方法研究[D]. 西安: 西北工业大学, 2008.
[7]
刘晓伟 火箭基组合循环(RBCC)动力宽适用性进气道研究[D]. 西安: 西北工业大学, 2010.
[8]
石磊, 何国强, 秦飞,等. 某RBCC 样机进气道的设计与数值模拟[J]. 航空动力学报, 2011, 26 (8): 1801- 1807.
[9]
吴亚可, 何国强, 刘佩进,等. 侧向收缩比对 RBCC 侧压式进气道起动性能的影响[J]. 弹箭与制导学报, 2011, 31 (3): 146- 150.
[10]
吴亚可 RBCC引射模态一次火箭调节和二次燃料喷注规律研究[D]. 西安: 西北工业大学, 2011.
[11]
GORDON S, MCBRIDE B J. Computer program for calculation of complex chemical equilibrium compositions and applications: NASA RP 1311 [R]. [S.l.]:[s.n.], 1994.
[12]
GORDON S, MCBRIDE B J. Thermodynamic data to 20 000 K for monatomic gases. NASA/TP-1999-208 523[R]. [S.l.]:[s.n.], 1999.
[13]
Herrmann CD, Koschel W W. Experimental investigation of the internal compression inside a hypersonic intake: ΑΙΑΑ 2002-4130[R]. [S.l.]: AIAA, 2002.
Outlines

/