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等离子体强化混合燃气燃烧研究

Study on the Plasma Enhancing Combustion of Mixed Gas
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摘要 为验证等离子体对固冲发动机中气相组分燃烧的强化特性, 通过建立等离子体助燃理论模型, 对有无等离子体条件下的混合燃气在固冲补燃室中的燃烧过程进行了数值和实验研究.研究结果表明: 在燃烧室中加入等离子体后, 有效促进了混合燃气的链式反应, 缩短了燃烧时间; 等离子体显著提高了混合燃气的燃烧效率, 燃烧效率增加了16.6%.与实验结果对比可知, 数值计算结果误差在10%以内, 说明所建立的理论模型较为准确地模拟了混合燃气燃烧过程, 具有一定的可靠性. In order to verify the enhancement characteristics of plasma in gas-phase combustion of the solid ramjet rocket, Numerical and experimental studies were carried out by establishing a theoretical model of plasma-assisted combustion. The result indicated that: the addition of plasma in the combustion chamber effectively promoted the chain reaction of the mixed gas and shortens the burning time; the plasma significantly increased the combustion effi.ciency of the mixed gas, and the combustion efficiency increased by 16.6%.Compared with the experimental results,the error of numerical calculation was less than 10% which indicated that the theoretical model was relative accurate.ly simulate the combustion process of mixed gas and has a certain reliability.
作者 纪海龙 冯喜平 JI Hailong1 ,FENG Xiping2(1. China Airborne Missile Academy,Luoyang Henan 471009;2.Key Laboratory of Combustion, Flow and Thermal-Structure,Northwestern Polytechnical University,Xi'an Shaanxi 71007)
出处 《河南科技》 2018年第10期139-142,共4页 Henan Science and Technology
关键词 等离子体 混合燃气 固冲发动机 燃烧效率 plasma;mixed gas;the solid ramjet rocket;the combustion efficiency
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  • 1柴玉萍,张同来.国内外复合固体推进剂燃速催化剂研究进展[J].固体火箭技术,2007,30(1):44-47. 被引量:25
  • 2Besser H. L. Strecker R. Overview of Boron Ducted Rocket Development During the Last Two Decades, J. of Propulsion and Power, Vol. 7 No. 2,Jan. - Feb. 1991:133 - 178.
  • 3Liu T. K. Effect of Fluorinated Graphite on Combustion of Boron and Boron Baseel Fuel Rich Fropellants,J. of Propulsion and Power, Vol. 12,No. 1, 1996:26 -33.
  • 4Liu T. K. et al. Effect of boron particle surface coating on combustion of solid propellants for dueted rockets.Propellants, Explosives, Pyrotechnics, 16: 156(1991).
  • 5Komai Iwao, Kubota Naminosuke.Gas generating propellants for ducted rockets. Proceedings of the International pyrotechnics Seminar 2001,28th: 425-430.
  • 6Strecker Rudiger, Harrer Alois. Composite solid propellant with a metal/inorganic fluoride admixture or a stable burning rate. USP 5, 143:566.
  • 7Hatcher Richard C. , Stephens William D. , Stanley, Robert L. Solid fuel gas generator for ducted rocket engine. USP6258188, 2001, 7.
  • 8Fawls, Christopher J. , Fields, Joel P. , Wagaman, Kerry L. Propellants and explosives with flouro-organic additives to improve energy release efficiency. USP6 843 868 , 2005.
  • 9MATHUR T,LIN K C,KENNEDY P.Liquid JP-7 combustion in a scramjet combustor[R].AIAA-2000-3581.
  • 10TAKESHI Kanda,NOBUO Chinzei.Dual-mode operation in a scramjet combustor[R].AIAA 2001-1816.

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