层流
机械
起爆
材料科学
加速度
管(容器)
爆燃
计算机模拟
层流火焰速度
火焰结构
计算流体力学
爆燃转爆轰
预混火焰
复合材料
化学
爆炸物
燃烧
经典力学
燃烧室
物理
有机化学
作者
Nobuyuki Tsuboi,A. Koichi Hayashi,Yoshikazu Tamauchi,Takashi Kodama
出处
期刊:Transactions of the Institute of Aviation
日期:2021-12-01
卷期号:2021 (4): 41-52
被引量:1
标识
DOI:10.2478/tar-2021-0021
摘要
Abstract The Artificial Thickened Flame (ATF) method, which involves artificially increasing the flame thickness so as to simulate with a coarse grid resolution, is applied to reduce the computational cost of predicting the Deflagration to Detonation Transition (DDT) in a tube with repeated obstacles. While simulation results depended on the parameter N (the number of grid points in laminar flame thickness), it was found that N values of more than 10 may be excessive. The results show that the chosen simulation method predicts the flame speed as compared to a reference experiment and captures the detail of the strong ignitions near the corner between the obstacle and the sidewall. The present simulation also captures the wrinkle flame front structure during the acceleration of flame.
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