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突跃型与平滑型斜爆震波起爆机制数值模拟

韩旭 周进 林志勇 刘世杰

韩旭, 周进, 林志勇, 刘世杰. 突跃型与平滑型斜爆震波起爆机制数值模拟[J]. 航空动力学报, 2012, 27(12): 2674-2680.
引用本文: 韩旭, 周进, 林志勇, 刘世杰. 突跃型与平滑型斜爆震波起爆机制数值模拟[J]. 航空动力学报, 2012, 27(12): 2674-2680.
HAN Xu, ZHOU Jin, LIN Zhi-yong, LIU Shi-jie. Initiation mechanism investigation of saltation and smoothness oblique detonation waves[J]. Journal of Aerospace Power, 2012, 27(12): 2674-2680.
Citation: HAN Xu, ZHOU Jin, LIN Zhi-yong, LIU Shi-jie. Initiation mechanism investigation of saltation and smoothness oblique detonation waves[J]. Journal of Aerospace Power, 2012, 27(12): 2674-2680.

突跃型与平滑型斜爆震波起爆机制数值模拟

基金项目: 国家自然科学基金(NSFC90816016,NSFC91016028)

Initiation mechanism investigation of saltation and smoothness oblique detonation waves

  • 摘要: 采用带有化学反应的Euler方程,对突跃型与平滑型2种形态的斜爆震波(ODW)在起爆机制和结构特点等方面的差异进行了研究.结果表明:斜激波(OSW)后是否存在亚声速区是判定斜爆震形态的依据.当波后火焰抬升斜激波面使得亚声速区存在时,横向激波与三波点结构就会出现并形成突跃型斜爆震.当波后所有区域皆为超声速区时,波后火焰燃烧无法影响到上游激波面,则会形成平滑型斜爆震.通过斜激波关系式给出了横向激波形成所需的临界斜激波角度,只有当斜激波角度大于此临界角度时才能形成突跃型斜爆震波,反之则形成平滑型斜爆震波.

     

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出版历程
  • 收稿日期:  2011-09-07
  • 刊出日期:  2012-12-28

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