摘要
为了研究射流入射压力对环形激波聚焦爆震起爆的影响,以氢气和空气混合物为例,对不同射流入射压力下环形激波聚焦爆震起爆过程进行了数值模拟,结果表明,当环形射流入射强度足够大时,其形成的激波聚焦能够形成高温、高压区域,从而直接起爆爆震波;爆震管推力壁对激波具有反射加强作用,有助于爆震波的形成;环形射流入射压力存在一个临界值,低于此值时,则不能起爆爆震波.
In order to investigate the influence of jet pressure on detonation initiation via imploding annular shock waves,detonation initiation with different jet pressures was simulated with hydrogen-air mixture.The results indicate that,when jet pressure is high enough,imploding annular shock waves can form high pressure and high temperature region that lead to direct initiation;thrust wall can strengthen reverberation shock,which contributes to initiate detonation;when the jet pressure is lower than its critical value,detonation can not be initiated.
出处
《航空动力学报》
EI
CAS
CSCD
北大核心
2010年第9期1964-1970,共7页
Journal of Aerospace Power
基金
空军工程大学学术基金(XS0901009)
关键词
脉冲爆震发动机
爆震起爆
爆震波
环形激波
数值模拟
pulse detonation engine detonation initiation detonation wave annular shock waves numerical simulation