Detailed features of one-dimensional detonations

被引:24
作者
Daimon, Y [1 ]
Matsuo, A [1 ]
机构
[1] Keio Univ, Dept Mech Engn, Kouhoku Ku, Kanagawa 2238522, Japan
关键词
D O I
10.1063/1.1526698
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The oscillation mechanism and reignition process of one-dimensional unsteady detonations are numerically studied using a one-step chemical reaction model governed by Arrhenius kinetics. A series of simulations, without perturbations from the outflow boundary to the detonation front, are carried out while the degree of overdrive, f, is varied between 1.10 and 1.74 (f = D-2 /D-CJ(2); where D is detonation velocity). Shock pressure histories and x-t diagrams are utilized in order to attain precise understanding of the one-dimensional unsteady detonations. At higher degrees of overdrive, f = 1.40-1.74, shock pressure histories agree with those of previous studies. The oscillation mechanism is the same as that of the large-disturbance regime of unsteady shock-induced combustion around a projectile. At lower degrees of overdrive, f<1.30, grid resolution affects the eventual results, because half reaction time in the shock pressure exhibits considerable variation. Four typical kinds of oscillation pattern are discussed and are explained by their x-t diagrams and shock pressure histories. Each oscillation mechanism is essentially the same as that of the large-disturbance regime. The reignition process in the failed regime was numerically investigated at f = 1.01-1.25. The reignition points tend to converge on a specified point in study of grid refinement, although the oscillation of the shock pressure histories becomes chaotic, suggesting the existence of a unique solution for reignition. All the simulation results for f = 1.01-1.20 show the failed regime after initial disturbance at the early stage. The failed regime is compared with the solution of the Riemann problem, and analysis consisting of a Rayleigh line for weak leading shock and a partially burnt Hugoniot curve is adopted. Analysis suggests the concept of partial chemical heat release, indicating the possibility of discontinuous change in conditions, and, indeed, simulation indicates occurrence of explosion. The explosion time derived from the analysis agrees well with the results of simulation. (C) 2003 American Institute of Physics.
引用
收藏
页码:112 / 122
页数:11
相关论文
共 20 条
[1]   THEORY OF UNSTABLE ONE-DIMENSIONAL DETONATIONS [J].
ABOUSEIF, GE ;
TOONG, TY .
COMBUSTION AND FLAME, 1982, 45 (01) :67-94
[2]   THEORETICAL AND NUMERICAL STRUCTURE FOR UNSTABLE ONE-DIMENSIONAL DETONATIONS [J].
BOURLIOUX, A ;
MAJDA, AJ ;
ROYTBURDS, V .
SIAM JOURNAL ON APPLIED MATHEMATICS, 1991, 51 (02) :303-343
[3]   STABILITY OF IDEALIZED ONE-REACTION DETONATIONS [J].
ERPENBECK, JJ .
PHYSICS OF FLUIDS, 1964, 7 (05) :684-696
[4]   FLOW CALCULATIONS FOR PULSATING 1-DIMENSIONAL DETONATIONS [J].
FICKETT, W ;
WOOD, WW .
PHYSICS OF FLUIDS, 1966, 9 (05) :903-&
[5]   THE DYNAMICAL LIMIT OF ONE-DIMENSIONAL DETONATIONS [J].
HE, LT ;
LEE, JHS .
PHYSICS OF FLUIDS, 1995, 7 (05) :1151-1158
[6]   Numerical resolution of pulsating detonation waves [J].
Hwang, P ;
Fedkiw, RP ;
Merriman, B ;
Aslam, TD ;
Karagozian, AR ;
Osher, SJ .
COMBUSTION THEORY AND MODELLING, 2000, 4 (03) :217-240
[7]   Flow features of shock-induced combustion around cylindrical projectiles [J].
Kamiyama, Y ;
Matsuo, A .
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2000, 28 :671-677
[8]   CALCULATION OF LINEAR DETONATION INSTABILITY - ONE-DIMENSIONAL INSTABILITY OF PLANE DETONATION [J].
LEE, HI ;
STEWART, DS .
JOURNAL OF FLUID MECHANICS, 1990, 216 :103-132
[9]  
LEHR HF, 1972, ASTRONAUT ACTA, V17, P549
[10]   Numerical investigation of the one-dimensional piston supported detonation waves [J].
Matsuo, A ;
Fujii, K .
ENERGY CONVERSION AND MANAGEMENT, 1997, 38 (10-13) :1283-1295