TY - JOUR
T1 - Numerical investigations on detonation propagation in a two-dimensional curved channel
AU - Sugiyama, Yuta
AU - Nakayama, Yoshio
AU - Matsuo, Akiko
AU - Nakayama, Hisahiro
AU - Kasahara, Jiro
N1 - Funding Information:
This work was supported by JSPS KAKENHI Grant Number 24246137.
Publisher Copyright:
Copyright © Taylor & Francis Group, LLC.
PY - 2014/11/2
Y1 - 2014/11/2
N2 - This article presents numerical results of detonation in a two-dimensional curved channel in order to discuss its propagation behavior and the stable propagation limit. We simulated the detonation with various channel widths in two types of the ratios of inner and outer radii (Rout/Rin), which are 1.5 and 2. Two propagation modes, named as marginal and stable modes, were observed. In marginal mode, curved detonation propagates with repetition of decay, re-ignition, and propagation. Its velocity varies from underdriven to overdriven in one cycle. In a stable mode, the detonation propagates steadily while keeping a curved shock front structure and a constant detonation velocity in the circumferential direction. The idea of quasi-steady solution to the numerical results is applied for stable detonation limit. We confirmed that the detonation propagates steadily in the case that a shock radius of the detonation front is larger than the critical value of quasi-steady solution. ©
AB - This article presents numerical results of detonation in a two-dimensional curved channel in order to discuss its propagation behavior and the stable propagation limit. We simulated the detonation with various channel widths in two types of the ratios of inner and outer radii (Rout/Rin), which are 1.5 and 2. Two propagation modes, named as marginal and stable modes, were observed. In marginal mode, curved detonation propagates with repetition of decay, re-ignition, and propagation. Its velocity varies from underdriven to overdriven in one cycle. In a stable mode, the detonation propagates steadily while keeping a curved shock front structure and a constant detonation velocity in the circumferential direction. The idea of quasi-steady solution to the numerical results is applied for stable detonation limit. We confirmed that the detonation propagates steadily in the case that a shock radius of the detonation front is larger than the critical value of quasi-steady solution. ©
KW - CFD
KW - Curved channel
KW - Detonation
KW - Geometry effect
KW - Propagation behavior
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U2 - 10.1080/00102202.2014.935621
DO - 10.1080/00102202.2014.935621
M3 - Article
AN - SCOPUS:84907789946
SN - 0010-2202
VL - 186
SP - 1662
EP - 1679
JO - Combustion Science and Technology
JF - Combustion Science and Technology
IS - 10-11
ER -