入射喷口宽度对环形射流激波聚焦起爆爆震的影响分析  

Investigation on the influence of jet width on detonation initiation via imploding annular shock waves

作　　者：曾昊[1] 何立明[1] 章雄伟[1] 李海鹏[1] 

机构地区：[1]空军工程大学工程学院,陕西西安710038

出　　处：《空气动力学学报》2011年第4期501-507,共7页Acta Aerodynamica Sinica

基　　金：空军工程大学学术基金(XS0901009)

摘　　要：为了研究射流入射喷口宽度对环形激波聚焦爆震起爆的影响,本文以氢气和空气混合物为例,对不同射流入射喷口宽度的环形激波聚焦爆震起爆过程进行了数值模拟,结果表明,当入射温度为一定值时,不同宽度的环形射流入射喷口对应着不同入射压力pin的临界值,当pin大于该临界值时,其形成的激波聚焦才能够形成高温、高压区域,从而起爆爆震波;随着入射喷口宽度的增加,射流的入射强度增大,其对应的临界入射压力随之减小。In order to investigate the influence of jets width on detonation initiation via imploding annular shock waves,detonation initiation with different jets width were simulated and hydrogen-air mixture was used.The results indicate that when jets temperture is constant,different jets width exist different critical jets pressure,when jets pressure pin is higher than the critical jets pressure,imploding annular shock waves can form high pressure and high temperature region that lead to direct initiation;the critical jets pressure decreased with the increase of jet width.

关 键 词：爆震起爆 爆震波 环形激波 

分 类 号：V211.3[航空宇航科学与技术—航空宇航推进理论与工程]