The re-initiation mechanism of detonation diffraction in a weakly unstable gaseous mixture

被引:23
作者
Shi, Lisong [1 ]
Uy, Ken Chun Kit [1 ]
Wen, Chih Yung [1 ]
机构
[1] Hong Kong Polytech Univ, Div Aeronaut & Aviat Engn, Dept Mech Engn & Interdisplinary, Kowloon, Hong Kong, Peoples R China
基金
中国国家自然科学基金;
关键词
detonation waves; TIME CONSERVATION ELEMENT; STABILITY; TRANSMISSION; SIMULATIONS; LAWS; WAVE;
D O I
10.1017/jfm.2020.311
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Numerical simulations were performed to investigate the re-initiation mechanism of a diffracted detonation wave near the critical channel width for a weakly unstable gas. Two scenarios were examined: diffraction of a planar detonation wave and of a cellular detonation wave inside the inlet channel. The results revealed that the critical channel width predicted using a cellular detonation wave is smaller than that predicted using a planar detonation wave. The re-initiation mechanisms are described in detail by tracing massless particles along both the plane of symmetry and the re-initiation path. For planar detonation diffractions, a compression wave is formed in the far field behind the diffracted shock. Re-initiation is closely related to the amplification of this compression wave and its coalescence with the diffracted shock. Depending on the inlet channel width, the strength of the reflected rarefaction wave is responsible for weakening the strength of the compression wave and its coalescence with the diffracted shock, consequently hindering the reaction of particles behind the diffracted shock wave. In cellular cases, the continuous collisions of transverse waves, which generate local explosion sites, sustain detonation wave propagation.
引用
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页数:36
相关论文
共 47 条
[1]   A numerical study of detonation diffraction [J].
Arienti, M ;
Shepherd, JE .
JOURNAL OF FLUID MECHANICS, 2005, 529 :117-146
[2]   Reaction zones in highly unstable detonations [J].
Austin, JM ;
Pintgen, F ;
Shepherd, JE .
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2005, 30 :1849-1857
[3]  
Benedick W., 1984, PROGR ASTRONAUTICS A, V94, P546, DOI DOI 10.2514/5.9781600865695.0546.0555
[4]   Effect of gaseous oxidizer composition on the detonability of isooctane-air sprays [J].
Benmahammed, Mohamed Amine ;
Veyssiere, Bernard ;
Khasainov, Boris A. ;
Mar, Modou .
COMBUSTION AND FLAME, 2016, 165 :198-207
[5]   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
[6]   THE METHOD OF SPACE-TIME CONSERVATION ELEMENT AND SOLUTION ELEMENT - A NEW APPROACH FOR SOLVING THE NAVIER-STOKES AND EULER EQUATIONS [J].
CHANG, SC .
JOURNAL OF COMPUTATIONAL PHYSICS, 1995, 119 (02) :295-324
[7]   Detailed features of one-dimensional detonations [J].
Daimon, Y ;
Matsuo, A .
PHYSICS OF FLUIDS, 2003, 15 (01) :112-122
[8]  
Desbordes D., 1993, Progress in Astronautics and Aeronautics, V153, P347, DOI [10.2514/5.9781600866265.0347.0359, DOI 10.2514/5.9781600866265.0347.0359]
[9]   DIFFRACTION OF A PLANAR DETONATION-WAVE AT AN ABRUPT AREA CHANGE [J].
EDWARDS, DH ;
THOMAS, GO ;
NETTLETON, MA .
JOURNAL OF FLUID MECHANICS, 1979, 95 (NOV) :79-&
[10]   Detonation wave diffraction in H2-O2-Ar mixtures [J].
Gallier, S. ;
Le Palud, F. ;
Pintgen, F. ;
Mevel, R. ;
Shepherd, J. E. .
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2017, 36 (02) :2781-2789