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Analysis of Micro-scale Flame Structure of AP/HTPB Base Bleed Propellant Combustion 被引量:2

Analysis of Micro-scale Flame Structure of AP/HTPB Base Bleed Propellant Combustion
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摘要 A complex multiple flame structure is formed during the combustion of AP/HTPB base bleed propellant.The AP monopropellant flame is concentrated in a thin zone above the burning surface of AP crystal to maintain self-sustained decomposition.Due to the low temperature near the burning surface,the diffusion between the decomposition products of AP and the pyrolysis products of HTPB occurs,and a partly pre-mixed diffusion flame structure-leading edge flame(LEF)is formed.The effects of pressure,chemical reaction rate and AP particle size on diffusion flame structure in the range from 20 atm to 100 atm are discussed.The Peclet number increases from 6.64 at 20 atm to 21.91 at 100 atm when AP particle size is 140 mm.The high temperature zone is blown away from the burning surface because the convective transport rate increases with the increase in Peclet number.The chemical reaction rate is enhanced and the diffusion mixing is inhibited as Damkohler number increases.The chemical heat release is more concentrated and the chemical reaction zone becomes narrow when Damkohler number changes from 330 at20 atm to 4700 at 100 atm.When AP particle diameter is decreased to 60 mm,the diffusion time scale is reduced due to the reduced diffusion length scale.So the diffusion mixing is enhanced and a more pre-mixed flame is formed.The burning rate increases because the more pre-mixed heat release increases the heat feedback to the HTPB binder. A complex multiple flame stracture is formed dining the combustion of AP/HTPB base bleed propellant. The AP monopropellant flame is concentrated in a thin zone above the burning surface of AP mystal to maintain seK-sustained decomposition. Due to the low temperature near the burning surface, the diffusion between the decomposition products of AP and the pyrolysis products of HTPB occurs, and a partly pre-mixed diffusion flame stracture-leading edge flame (LEF) is formed. The effects of pressure, chemical reaction rate and AP particle size on diffusion flame structure in the ravage from 20 arm to 100 ann are discussed. The Peclet number increases from 6.64 at 20 ann to 21.91 at 100 ann when AP particle size is 140 μm. The high temperature zone is blown away from the burning surface because the convective transport rate increases with the increase in Peclet number. The chemical reaction rate is enhanced and the diffusion mixing is hlhibit ed as Damkolfler nunlber increases. The chemical heat release is more concentrated axed the chemical reaction zone becomes nan'ow when Damkolfler nunlber changes from 330 at 20 ann to 4700 at 100 atm. When AP particle diameter is decreased to 60 μm, the diffusion time scale is reduced due to the reduced diffusion length scale. So the diffusion mLxing is enhanced a more pre-mixed flame is formed. The burning rate increases because the more pre-mixed
出处 《Defence Technology(防务技术)》 SCIE EI CAS 2013年第4期217-223,共7页 Defence Technology
基金 the financial support provided by the National Natural Science Foundation of China(No.51176076)
关键词 推进剂燃烧 火焰结构 HTPB 结构分析 AP 底排 化学反应速率 Peclet数 AP/HTPB Base bleed charge Harne structure Pec1et number Damkohler number
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  • 1张炎清,赵子华.底部排气弹底排装置点火过程对距离散布的影响[J].弹道学报,1994,6(1):53-56. 被引量:13
  • 2郭希福.底排弹外弹道学[M].北京:兵器工业出版社,1998..
  • 3郭希福,底排弹外弹道学,1998年
  • 4《化学工程手册》编委会,化学工程手册,1980年
  • 5郭锡福.底排弹外形弹道学[M].北京:兵器工业出版社,1998..
  • 6郭锡福.底部排气外弹道学[M].北京:国防工业出版社.1995.
  • 7Jeong-Yeol Choi,Edward Shin. Numerical study of base-bleed projectile with external combustion [ C ] //41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 10 - 13 July 2005 ,Tucson, Arizoba.
  • 8Makoto Kohga, Saeko Yoshida. Burning rate characteristics of AP- based composite propellant using bimodal AP [ C ] //42nd AIAA/ ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 9 - 12 July 2006, Sacramento, California.
  • 9Ciepluch C C. Spontaneous reignition of previously extinguished solid propellants[ R]. NASA TN D-2167,1964.
  • 10Merkle C L,Turk S L,Summenfield M. Extinguishment of solid propellant by rapid depressurization[ C] //Dept. of Aerospace and Mechanical Sciences,Princeton Univ. , N. J. ,AMS Rept. 880,July 1969.

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