The diffusion flame structure of an ammonium perchlorate based composite propellant at elevated pressures

被引:20
作者
Hedman, T. D. [1 ]
Groven, L. J. [1 ]
Cho, K. Y. [1 ]
Lucht, R. P. [1 ]
Son, S. F. [1 ]
机构
[1] Purdue Univ, Dept Mech Engn, Maurice J Zucrow Labs, W Lafayette, IN 47906 USA
关键词
Ammonium perchlorate; Hydroxyl-terminated polybutadiene; Planar laser induced fluorescence; Composite propellant; Flame structure; SURFACE-STRUCTURE; TEMPERATURE; COMBUSTION;
D O I
10.1016/j.proci.2012.06.171
中图分类号
O414.1 [热力学];
学科分类号
摘要
Examination of the surface behavior and flame structure of a bimodal ammonium perchlorate (AP) composite propellant at elevated pressure was performed using high speed (5 kHz) planar laser-induced fluorescence (PLIF) from 1 to 12 atm and visible surface imaging spanning 1-20 atm. The dynamics of the combustion of single, coarse AP crystals were resolved using these techniques. It was found that the ignition delay time for individual AP crystals contributed significant to the particle lifetime only at pressures below about 6 atm. In situ AP crystal burning rates were found to be higher than rates reported for pure AP deflagration studies. The flame structure was studied by exciting OH molecules in the gas phase. Two types of diffusion flames were observed above the composite propellant: jet-like flames and v-shaped, inverted, overventilated, flames (IOF) lifted off the surface. While jet-like diffusion flames have been imaged at low pressures and simulated by models, the lifted IOFs have not been previously reported or predicted. The causes for the observed flame structures are explained by drawing on an understanding of the surface topography and disparities in the burning rates of the fuel and oxidizer. (C) 2012 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
引用
收藏
页码:649 / 656
页数:8
相关论文
共 24 条
[1]   CARS PROBE OF RDX DECOMPOSITION [J].
ARON, K ;
HARRIS, LE .
CHEMICAL PHYSICS LETTERS, 1984, 103 (05) :413-417
[3]   AMMONIUM-PERCHLORATE COMBUSTION - EFFECTS OF SAMPLE PREPARATION - INGREDIENT TYPE - AND PRESSURE, TEMPERATURE AND ACCELERATION ENVIRONMENTS [J].
BOGGS, TL ;
ZURN, DE ;
NETZER, DW .
COMBUSTION SCIENCE AND TECHNOLOGY, 1973, 7 (04) :177-183
[4]   SURFACE STRUCTURE OF AMMONIUM PERCHLORATE COMPOSITE PROPELLANTS [J].
BOGGS, TL ;
DERR, RL ;
BECKSTEAD, MW .
AIAA JOURNAL, 1970, 8 (02) :370-+
[5]   An elementary discussion of propellant flame geometry [J].
Buckmaster, J ;
Jackson, TL ;
Yao, J .
COMBUSTION AND FLAME, 1999, 117 (03) :541-552
[6]   Flame structure and burning rate of ammonium perchlorate/hydroxyl-terminated polybutadiene propellant sandwiches [J].
Chorpening, BT ;
Knott, GM ;
Brewster, MQ .
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2000, 28 :847-853
[7]  
Eckbreth A.C., 1991, INT J ENERG MAT CHEM, V3, P115
[8]   LASER-INDUCED FLUORESCENCE IN HIGH-PRESSURE SOLID-PROPELLANT FLAMES [J].
EDWARDS, T ;
WEAVER, DP ;
CAMPBELL, DH .
APPLIED OPTICS, 1987, 26 (17) :3496-3509
[9]   Diffusion flame calculations for composite propellants predicting particle-size effects [J].
Gross, Matthew L. ;
Beckstead, Merrill W. .
COMBUSTION AND FLAME, 2010, 157 (05) :864-873
[10]   Diffusion Flame Calculations for Composite Propellants Using a Vorticity-Velocity Formulation [J].
Gross, Matthew L. ;
Beckstead, Merrill W. .
JOURNAL OF PROPULSION AND POWER, 2009, 25 (01) :74-82